Aircraft Landing Gear Design Optimization Using Advanced Engineering Software Case Study

Stress Analysis and Material Selection for Enhanced Landing Gear Performance

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Chapter 1: Introduction

In this final report, the work begins with “The optimization of gear landing.” This particular report, there is used software work with the help of “Solid works and the Abaqus” platform. Nowadays the “landing gears” play a huge compact role for planes also for jets. There is needed great efficacy to maintain the gear landings in an effective way. Depending on the integrity of the structure planes are allowed to land in a well and safe way. The overall work is done to know the optimization of the gear landings. The design, stress for the landings, and loads on the model are the suggested points to work on in this report. The choice of material is also discussed in a huge way also the technologies to conduct this report. This is the overall introduction to “the optimization for gear landings.” With the help of the introduction chapter there is done great establishment of the “background of the study” for “the optimization for gear landings.” Also, there is done the establishment of a compact section regarding the aim of the research, the objectives of the procedure of research, the several kinds of the truthfulness of objectives, the compact questions that need to be solved for this report, the rationale also the significance for “the optimization for gear landings” elaborate here. Then there is done a compact research framework. At last, the segment of the conclusion for the chapter on induction to establish the “optimization for gear landings” in a sustainable way.

1.1 Background of the Study

The “background of the study” focused on “the optimization for gear landings.” The study focuses on the most common and important section of the aircraft. This study focuses greatly on the “landing gears.” Because the failures of the selective model are able to harm the overall aircraft also it is harmful to people also. For this reason, the great work through Solidworks and Abaqus software with two different material properties will choose to make a compact comparison of which material is the sustainable choice with stress analysis. To reduce the failures several kinds of strategies are used in this report. This is the compact background of the study for “the optimization for gear landings.”

1.2 Research Aim

The main aim of this report is to establish “the optimization for gear landings” in a compact way with the help of Solidworks and the Abaqus software platform. The aim section also focused on the process of stress analysis depending on two several materials [9]. The alloy steel and aluminum alloy 7079 is the choosable materials to make the comparison. Depending on the behaviors of the materials stress analysis is also able to show different result segments. The modeling through Solid works software and the establishment of Stress analysis through the Abaqus platform also is focusable aims in this report. These all are the sustainable research aim for “the optimization for gear landings.” Depending on the research aim the whole work is conducted in this particular assignment. The aim helps the optimization of gear landing in an effective way. Then aim also focus to conduct the perfect simulation result also.

1.3 Research Objective

• To know the compact material for “the optimization for gear landings.”
• To know the Design modeling of “the gear landings.”
• To know the compact stress analysis for “the optimization for gear landings.”
• To know the good establishment of judgments in an effective way.
• To know the importance of gear landings for the aircraft.
• To know the systemic way for the gear landings.

1.4 Research Questions

1. Is Alloy steel a sustainable choice for gear landings?
2. Is aluminum alloy 7079 the good choice for the gear landings?
3. Is the stress simulation the sustainable choice for analysis?
4. Is secureness of gear landings needed?
5. Is the gear landings important for the Aircraft?

1.5 Research Rationale

The main purpose of “the landing gears” in the segment of aircraft is basically implemented for the purposes of giving compact systems regarding suspension during the purpose of take-off and also for landings. The research rationale also focuses on the compact design of the selective model to recognize the structural design also the analysis of stress. The purpose of “dissipating the kinetic energy” or the purpose of landing impact also is the sustainable rationale for this individual report [10]. The rationale can say that the process of decreasing the overall impact regarding loads able to transmit in the airframe. The rationale part is so much important because everyone can know about the importance of the “optimization for gear landings.” The designing process for the establishment of the model and the stress analysis through the Abaqus platform is able to provide the sustainable rationale for this particular report in a great way.

1.6 Research Significance

The significance of the research process also focuses in a great way on “the optimization for gear landings.” As a significance, it can be said that the gear landing able to allow compact forceful applications with the segment of breaks in the time of landings with high speeds [11]. The significance also can ensure that the structure of compact gear landing and the use of material need to have the compact static also fatigue strength, the stiffness in a high way, toughness in a good way, the resistance for the environment also able to established in a low-cost also in a low weight. Therefore the first with the help of Solid works there is provided the establishment of “landing gear structures.” then with the help of Abaqus software there is maintained the significance of the analysis of stress.

1.7 Research Framework

Figure 1: Research Framework

1.8 Conclusion

With the help of this part, there is done compact conclusion for the introduction chapter of “The optimization for gear landings.” The gear landings are used for the purpose in a primary way. Therefore the importance of this model is so much important for the system of the entire aircraft. To connect with the land through the gear landings are used. Therefore the modeling and design for the “gear landings” also the analysis process of stress also recognized in this report in a compact way. The chapter of introduction is able to introduce the project in an initiative way then the whole background is discussed for “optimization for gear landings.” All the parts of this chapter are able to meet the requirements. Therefore the brief discussion about the introduction chapter ends here in a compact way.

Chapter 2: Literature Review

2.1 Introduction

This segment is also an important chapter that is able to describe several aspects of the model also the several knowledge aspects of “The optimization for gear landings.” This particular chapter described such important things that help a lot with the implementation process in this particular project. The section on the empirical study is able to distribute such kinds of studies. Then the segment of the theories also the models give the aspects regarding this particular report. Then there is provide compact gaps in the literature. There is established a picture regarding the dependent variable and also the independent variable to conduct the picture of a conceptual framework.

2.2 Empirical Study

This particular segment there is established several papers regarding the selective topic. All these papers have several kinds of aspects on “the optimization of gear landing with solid works and abacus.” These papers help the implementation process in this particular dissertation file in a great way. Therefore, the sustainable and efficacy full studies are-

According to Hafid et al. 2020, in this particular work, an investigation in a mathematical way of the fuselage design of the LSU 05 NG was done. This structure is intended for payloads up to 25 kg. A static mathematical investigation is able to utilize the conduction of a limited component strategy was performed utilizing Simulia Abaqus [1]. The planned fuselage structure comprising casings, longitudinal individuals, and skins can be depicted as a semi-monocoque structure. This airframe utilizes a mix of balsa wood and her GRP composites as a material. There are three burden cases that are departure, the voyage also landing. The Tsai Slope Disappointment Measure is utilized to look at the strength of composite designs under applied loads. The most extreme pressure from this estimation is 49.24 MPa in ground conditions (departure as well as landing) and the greatest chief pressure during the journey is 52.76 MPa. The greatest Tsai Slope model is 0.95 in voyage conditions. These reproduction results show that the fuselage structure is as yet solid and a few parts can be upgraded, in this way lessening the heaviness of the airplane. Therefore, this particular study helps to gather knowledge about the choice of material.

According to Yousefi et al. 2023, The principle about to motivation behind this particular article is to affordable for “3D bio-enlivened auxetic meta structures imprinted” in the time of delicate/hard polymers for the purpose of “energy assimilation/dissemination applications” under one-off also for “cyclic pressure unwinding.” The selective megastructure was created in light of comprehension of the hyperplastic properties of thermoplastic polyurethane (TPU) polymers, and snowflake-enlivened plans got from the hypothesis and trial. Increment. The 3D megastructure is made by the innovation of MultiJet Combination 3D printing [2]. The possibility also the mechanical execution of several kinds of meta-structures is assessed tentatively way and mathematically way also. A computational limited component model (FEM) of the megastructure is created and approved tentatively. The testing procedure of Mechanical pressure of TPU auxetics showed enormous recoverable strain, mechanical hysteresis portrayed stress unwinding, by unequaled compressive burden dump bends, Mullins impact, cyclic pressure unwinding, and high energy retention/dissemination.

Figure: The responses of stress strain

One-of-a-kind qualities, for example, capacities are demonstrated. Mechanical trial of the Dad 12 megastructure additionally shows elastoplastic conduct with remaining strain and high energy ingestion/dispersal execution. The created FEM has been demonstrated and also shows the two have the option to reliably repeat the principal highlights seen in the trials. The material construction model, calculated plan, and results are supposed to contribute altogether to the 3D printing of tunable delicate and hard high-energy Meta devices as per need. Therefore this individual study also helps a lot for the progression of the implementation process in a great for “the optimization of gear landings with solid works and Abacus.”

According to MohamedZain et al. 2022, this paper able to portrays the plan of a little Unmanned Aerial Vehicle (UAV). 3D programming experience. The most simple and common way of building the parts of an outline incorporates numerous techniques to guarantee that the parts meet prerequisites while likewise fulfilling security and industry guidelines. The planning step starts with the determination of accessible materials for the robot that are polylactic corrosive (PLA) [3], acrylonitrile styrene acrylate (ASA), and acrylonitrile butadiene styrene (ABS). The robot outline comprises four principal parts: center top cover (50g), side top cover (10g), center cover (30g), and drone arm (80g). A recreation was rushed to decide the burdens, removals, and loads of the robot parts.

Figure: Result of stress and displacement

Furthermore, a compromised study was directed to settle the part calculation and different sources of info in the view of according need. The consequence of this new plan can be communicated in a plan idea in which two body parts, the focus cover and focus top cover, are joined utilizing a carabiner capability without the requirement for the extra clasp.

According to Oyesola et al. 2022, the purpose of assessing new classifications of advances, for example, added substance producing, and dissecting the effect of assembling processes on proficiency in a goal and quantifiable manner is significant. This study portrays the plan also the reproduction of a titanium combination (Ti6Al4V) bearing lodging utilizing specific laser liquefying (SLM). A limited component Investigation (FEA) strategy was utilized to assess the reasonableness of his Ti6Al4V for aviation applications [4]. The decision of Ti6Al4V depends on its near advantage in solidarity to-weight proportion. implied and express modules of Abaqus programming were utilized for nonlinear and straight examination of part parts. The outcomes acquired show that the titanium combination (Ti6Al4V) fulfills the plan, capability, and administration necessities of bearing lodging parts fabricated for aviation applications. The planned bearing is appropriate for fast and temperature applications above 1900K, however, the most extreme pressure prompted in the part during stacking was 521 kPa. Obviously, it was created. The pressure causes no distortion or deformity of the material with yield focuses in the scope of 820 MPa. This work mirrors his insight into material conduct under working circumstances to give plan information for creating bearing lodgings for his AM in his SLM innovation utilizing Ti6Al4V.

According to Gao et al. 2022, Molecule affidavit conduct is significant for further developing covering quality. In view of Euler and Lagrange's coupled strategy (CEL), a three-layered multi-molecule irregular statement model was developed and grain heterogeneity was brought into his TC18 substrate. A polycrystalline microstructural model of the warm shower substrate was created by the Voronoi technique. Changes in temperature, strain and stress fields during molecule affidavit were uncovered, and the development component of pore surrenders was likewise examined [5]. The outcomes show that the little grains have a huge all out strain and the enormous grains have a little center strain and a huge edge strain. The pressure esteem close to the huge grains of the covering is enormous, and the pressure at the edge of the covering is moderately little. The pressure dissemination in the TC18 substrate looks like a non-uniform and irregular mathematical conveyance of grains. In view of this, a reaction surface model of covering properties was made, the impact of cycle boundaries on covering properties was dissected, and the responsiveness of interaction still up in the air. This exploration can give establishment and direction to designing applications in related fields.

According to Zhang et al. 2023, Here, we utilized generative plan strategies to perform plan enhancement of the primary arrival gear (MLG) geography and harm resistance of a 19-traveler turboprop island-bouncing airplane. Generative plan innovation has changed how primary parts are intended to accomplish ideal part math while keeping up with underlying honesty to endure endorsed loads, both static and exhaustion. As the MLG armature is one of the super underlying components (PSEs) of an airplane, disappointment in this part can prompt disastrous mishaps. A harm resilience investigation is in this way compulsory to decide the help life and examination time frames valve [6]. Here, a blend of short-range and long-range airplane flights was utilized to create the heap spectra utilized for break development concentrates on equipment. By carrying out both geography advancement and harm resistance examination on the armature, the heaviness of the armature can be fundamentally diminished while keeping up with consistency with the static strength and harm resilience perspectives expected under the Government Obtaining Guideline (FAR) expected to be decreased by 23.

According to Brånäs and Enderby 2022, Saab Flight Airplane Primary Format Idea Configuration utilizes thickness streamlining to assess underlying design ideas. In light of the thickness esteems, the ideas can measure up to one another, and the best one grew further. Right now, the creation and assessment of underlying ideas are primarily done physically. Hence, research is in progress on the best way to carry out plan computerization.

Lessen this manual and dull work. This study is expected to rapidly investigate the plan space to track down a decent reason for new airplane improvement. This incorporates researching how to synchronize between Underlying Format Models (SLMs).

Further developed worldwide limited component model (GFEM). This paper adds to the examination by thinking about carrying out plan computerization in the formation of his SLMs connected with body structures. Also, execution of plan computerization in the readiness of GFEM is being considered to empower programmed assessment of ideas. This work likewise investigates how synchronization between models can be moved along. Adjusted and consolidated MOKA and RAD programming improvement approaches to structure the paper. The paper was acted in 3DEXPERIENCE programming, explicitly utilizing CATIA and SIMULIA applications. This paper gave a technique to creating and assessing theoretical plans for airplane structures utilizing plan mechanization. The new technique contains two models with relating scripts. The primary model created is a device for calculated originators that can make airframe SLMs from client-characterized inputs [7]. The subsequent model is produced by means of content and is a direct interface GFEM to SLM. In rundown, the created technique speeds up reasonable plan emphasess of fuselage structures contrasted with current strategies. Less detail, however more consistency and consistency. GFEM couldn't satisfy its motivation with the created strategy because of time imperatives and programming impediments. Nonetheless, the synchronization among SLM and GFEM was effectively carried out and incorporated exceedingly significant components.

According to Bal 2020, in the airplane business, fragile, low-edge configuration is a higher priority than any vehicle fabricate. This study portrays a plan guide for items expected for use in battle airplane and gives research models in our public writing. It was wanted to figure out what stacks this construction is exposed to because of contender moves and ecological circumstances. Weapon frameworks were chosen to act as an illustration of utilization, and the errands and methods of activity of suspension and trigger frameworks were depicted exhaustively. General writing and examination on ejector discharge units and weapons were surveyed to give data on underlying model and lighting studies. The contender movement and climate then determined the ejector discharge unit and firearm load [8]. Additionally, the power expected to securely eliminate these weapons from the airplane was portrayed and integrated into the interaction. A flexible and exchangeable burden structure for conveying air-to-endlessly air to-ground weapons with a similar trigger framework, which had not recently been applied, was thought of. The burden structure is displayed in the SolidWorks program as per your necessities.

2.3 Theories and Models

In this particular section, there is established a compact discussion about the process of theory to conduct the model. The sustainable choice is the theory of optimization. The theory of optimization is able to connect with the model. The selective model for this report is “gear landing.” Therefore, the theory of optimization with the modeling process through Solid works along with the analysis of stress through the Abaqus platform conducted here [12]. Therefore, it can be assured that the sustainable theory is d an optimization theory and the selective model is known as a “gear landing.” Therefore, this is the total optimization of “theories and models.”

2.4 Literature Gap

This section is a great section that is able to discuss the gap regarding the overall research process in a great way. The “rupture of hydraulic lines”., sometimes eros regarding the parts [13], the time took the matter of software work, and the segmentation and optimization of gear landings have so much unavailability to compile the research process. The compact choosable material behavior which one is better and which one is not so good cannot able to find in the literature section in a perfect way. The section literature is also not able to find the sustainable choice work software which is so much compact for this particular project [14]. Depending on the segment of the literature review many resources are gathered and find some gaps regarding the literature that all are able to implement for the purpose in the future.

2.5 Conclusion

In this particular section that can be said that all the points meet the requirements. The section of the Introduction first introduces the “literature review chapters” in a compact way. Then with the help of the section on empirical study established many different research papers according to the selected topic. All the papers were able to generate several aspects regarding the “Optimization of gear landings with solid works and abaqus.” This particular chapter also makes connectivity with the optimization theory along with the model of gear landing. Depending on the several empirical studies this section also conducts a perfect segment of literature gaps that are able to discuss the gaps in the research process. The picture of the conceptual framework depending on the independent variable and dependent variable also generate in this chapter perfectly utilizing way.

Chapter 3: Methodology

3.1 Introduction

This is the initial interface for the chapter on methodology. This particular chapter, there is created a great establishment of the methodology of “The optimization for gear landings.” With the help of the introduction part, there is able to come with a segment of the method outline. Then there is also the establishment of the positivism philosophy. There is also include the approach in an inductive way because the primary analysis process is conducted in this report. The design also strategy also included the establishment of methodology. There is conducted the primary analysis process therefore the secondary data collection method is the sustainable choice for this report. The ethics also limitations are done here to establish the methodology in a compact way. The chapter ends with a segment on concussions.

3.2 Method Outline

The particular segment regarding the outline of the method is able to describe “The optimization for gear landings” in this segment. There is used The Solidworks and the Abaqus platform to make the compact outline. The overall research process for “The optimization for gear landings” choose for making the design and also the analysis of stress for two different materials [15]. The comparison results are able to show the difference between the stresses and also able to explain which material is the sustainable choice in a great way. The innovation also has some build-up strategy conducted in this report to make the connectivity of method outline in a great way.

3.3 Research Philosophy

Several kinds of philosophy can be used for making the report in a compact way. The philosophy of realism, interpretivism, plagiarism, objectivism, and positivism are used for need purposes. For this report about “The optimization for gear landings,” the philosophy of positivism is the sustainable choice to conduct this overall report in a great way [16]. The Positivism philosophy is the sustainable choice because this philosophy is able to connect with accurate approaches, designs, and methods also for strategies. The philosophy is able to show the real work of modeling and design for the “gear landings.” the work of Abaqus also evaluates the positivism of stress analysis in a perfect way. A positive selection of materials is also needed to make the model sustainable way [17]. Therefore it can say that the philosophy of positivism is the sustainable choice for “The optimization for gear landings.”

3.4 Research Approach

The segment approach is so much important for every report. Two kinds of approaches can be used for the purpose of research. For this particular project, a sustainable choice is an inductive approach. The inductive approach here is used to increase the efficacy of “The optimization for gear landings.”

Figure: Approaches

The segmentation of the inductive approach is able to meet with the conclusion through the generating primary analysis process [18]. The approach in an inductive way is also known as “bottom-up” reasoning.

3.5 Research Design

It can be assured that the design of the research connects with the compact out coming result from the study in a scientific way. Several kinds of tools as well as techniques can be used for the processing of the research design in an initiative way. For the purpose of the conduct of this research, Solid works tools were used for the designing purpose [19]. When the designing and modeling are about to end then the model is used with the Abaqus tool for the purpose of Stress analysis. Depending on the Ally steel material and also the aluminum alloy material the analysis process is conducted in this particular research. The technology of software work is conducted in this particular report for the purpose of “the optimization of gear landing.” This kind of research design is known as a policy of quantitative research process [20]. Quantitative research is the sustainable choice because in this report the experimental research was conducted with the help of software work.

3.6 Research Strategy

The strategy of the whole research process means the process of conducting the study about “the optimization of gear landing.” The main strategy that focuses on this report that is- the software works through solid works and the Abaqus platform, and the behaviors of the materials according to the need. The compact segment of the designing process, measurement process [21], and perfect analysis with proper dimensions is the main strategy for “the optimization of gear landing.” The segment of stress is so much important to analyze in the gear landing so the analysis of stress also is a compact strategy regarding the research process.

3.7 Research Method

Several kinds of methods can be used for the purpose of the research of “the optimization of gear landing.” in this particular research the mono-method policy is used. The mono-method policy was conducted with the primary analysis process [22]. So the process of primary analysis with the mono method conduct “the optimization of gear landing” in a well way. The mono method connect with the quantitative primary analysis process. Therefore, this connectivity of the research method helps the process of data collection in a compact way.

3.8 The method of data collection

The compact process of data collection helps a lot with the analysis process. In this particular research process, the primary analysis process is created which means the data collection process connects in a secondary way. The “secondary data collection method” for the primary analysis is the sustainable choice for this individual report. The usefulness of the “solidworks with Abaqus [23]” software platform used for primary analysis can relate to the secondary data collection method in a compact way.

3.9 Research Ethics

The ethics regarding gear landing are conducted in this section. Several kinds of ethics are needed conduct to provide a sustainable model of gear landing with the process of optimization in a great way. The ethics must follow the compact stability for the purpose of take up and for a takedown. The quality of braking also for policies of steering [24], the compact length of the gear with the behaviors of material, and the stress segment of the material also needed to be focused in a great way. These all are compact ethics for “the optimization of gear landings.”

3.10 The limitations of research

The research process of “the optimization of gear landings” is also able to connect with the limitation segment effectively. That segment is able to focus on the weakness all over this study. Here is some legacy held during the collection the information from various sources [25]. The legacy regarding the slow software also sometimes occurred issues at the time of proceeding with the job. Therefore, this is the limitation of the research.

3.11 Conclusion

At the last, it can be said that with the help of a great introduction to the methodology, the compact outline of the method, the philosophy in a positive way, the approach in an inductive way, the quantitative design, technical strategy, the policy of mono method, the primary analysis process through secondary data collection method, some ethics also the limitation of the research able to described the “the optimization of gear landings” in a compact way with the designing through solidworks platform and the stress simulation through Abaqus conducted in the particular report to connects with the Analysis and findings of result segment compact way.

Chapter 4: Analysis and Findings of Result

4.1 Introduction

This is the important part of discussing the chapter “Analysis and findings of results” in a compact way. In this particular report the conduction of results for “the optimization of gear landings” is able to provide all of the results with the help of Solidworks software as well as Abaqus software in an effective way [26]. At first, the drawing, designing also modeling of “gear landing” was done with the help of Solidworks software. Then the compact model was imported into the Abaqus platform for the purpose of stress analysis. The Stress analysis depending on the separate behaviors of the material able to make the comparison of stress. Therefore, both selective software is used in a great way to conduct the primary analysis process to provide proper findings as a result.

4.2 Primary Analysis and Findings

Below Al the pictures are able to demonstrate the process of primary analysis with the proper results. Overall, all the results for “the optimization of gear loading” is generated with the help of proper work with the Solid works platform as well as with the Abaqus software platform.

The design of landing gear connects with the various requirements of “strength, stability, stiffness, ground clearance, control” These requirements help to proceed with operation alsop for safety purpose for the aircraft. Depending on the material properties cost-effectiveness is created. The mass production depends on the quality and design process.

Figure: Fillet used to create a model

The initial drawing here started with the help of the fillet option to create the gear-landing model. The yellow section is able to show the fillet option. Depending on the choice of the plane there is conducted the item for the model is an effective way.

Figure: Use of extrude boss base

There is used the option of extruding the boss base to generate the main structure of the model. The option of extruding the boss base is used to make the cross-section in effective way.

Figure: Use of plane

The use fullness of the right plane is used here to generate the geometry with a circle. The option of “extrude boss base” was used the make the structure in an initiative way.

Figure: Base

There is done the compact base of the model with the help of several options through the solid works platform [27].

Figure: Lower structure of gear landing

The above picture able to show the main body of the gear landing. The overall green section is assigned as the main body [28]. The lower structure of gear landing basically made with the extrude boss base option in an effective way.

Figure: Top View

This is the top view of the model. That is able to show the upper view of the great landing. The structure is about to end here with great aspects.

Figure: Main Body

With the help of several planes, boss extrude, cut extrude, and revolved boss base also with the fillet segment there is a compact main body of gear landing about to end here with compact measurements also with great design segmentation [29] [Refer to Appendix 1].

Figure: Material Properties

Above the picture able to shown the material properties of the model. Depending on the properties of material able to conduct the stress analysis process.

Figure: Instance

The red lines able to show that the instance created in a perfect w3ay. The selection is used to compile in the analysis process in an effective way.

Figure: Load

By this picture it can be assigned that the load generated applicable in this work perfect way.

4.3 Conclusion

In this section can be assured that the overall work of Solidworks to make the compact design of gear landing and the well establish stress analysis process are done in this chapter. Therefore the analysis process also helps to conduct the actual findings in a great way. The results with proper findings conducted in this particular chapter.

Chapter 5: Conclusion

5.1 Introduction

This is the final conclusion chapter that commits with several parts to discuss “the optimization of gear landings with the help of Solid works and Abaqus.” At the initial stage, there is afford ness of the objectives that all are linked in a proper way and demonstrated in this report in an accurate way. The section regarding recommendations for gear landing also evaluates in this assignment. In the end, there is held the compact generation of final conclusion.

5.2 Linking with Objectives

In this particular section there is provide a great revolution of overall objectives in a compact way with sustainable answers as per the need.

• To know the compact material for “the optimization for gear landings.”

It can be assured that both the materials “alloy steel and aluminum alloy” are the sustainable choice of material for the gear landing. But depending on the material properties and material behaviors also analyzing the stress the alloy steel is a more compact choice for making the gear landing. The stress simulation result is able to clarify this discussion in a compact way. The process regarding the optimization of gear landing with the compact material meets up with the findings in a compact way.

• To know the Design modeling of “the gear landings.”

The overall work through the solid works platform is able to show that the designing process also the modeling process are done in a compact for gear landing. With the help of three kinds of planes with several options for drawing purposes able to show the design modeling of the gear landing in a compact way.

• To know the compact stress analysis for “the optimization for gear landings.”

With the help of solid works drawing then the model was imported into the abaqus platform for the analysis of stress. The simulation results depending on two kinds of material properties able to show that “the optimization of gear landing” with the segment of compact stress the alloy steel is a more sustainable choice than the aluminum alloy. Therefore the whole model is able to provide results regarding stress.

• To know the good establishment of judgments in an effective way.

The overall software work is time taking matter that is done in a compact way with the possibilities of result segment, therefore, the judgment results can also show the efficacy of the gear landing in a compact aspect for the future segment.

• To know the importance of gear landings for the aircraft.

The landing gears are a necessary part of the aircraft. Therefore without this element, the aircraft are not able to take off and take down also for many other purposes. So the effectiveness of gear landing is so much important for the aircraft. The importance of gear landing is also able to produce a compact system of suspension. The design of gear Lansing generated for absorbing the kinetic energy to decrease the “impact loads transmitted to the airframe.”

• To know the systemic way for the gear landings.

The overall work through the designing process and the stress simulation process is done in a perfect systemic way for the purpose of gear landing. That means this objective also meets the requirements.

5.3 Recommendation

The overall work was done with the help of the solid works platform and with the abaqus platform. This project also can be created with the help of the Creo software platform. As well as several kinds of materials can be used for more stress analysis. Therefore, the work can be created in a more effective way if more accurately available on the online platform. Therefore, it also can be assured that The Ansys software also can be used for the stress simulation. The effectiveness of gear landing needs more efficacy to recover several kinds of accidents.

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Conclusion

In this final conclusion it can be assured that the overall assignment going to be end in an exact way with the possible effective result. The essential model that is gear landing created here with two several software platform. The solid works software use to create the design and at the end the Abaqus software use to compile the3 results of stress simulation in an effective way. Therefore, the project t meets with the requirement in an effective way.

References

Journals

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Yousefi, A., Jolaiy, S., Lalegani Dezaki, M., Zolfagharian, A., Serjouei, A. and Bodaghi, M., 2023. 3D?Printed Soft and Hard Meta?Structures with Supreme Energy Absorption and Dissipation Capacities in Cyclic Loading Conditions. Advanced Engineering Materials, 25(4), p.2201189.

MohamedZain, A.O., Chua, H., Yap, K., Uthayasurian, P. and Jiehan, T., 2022. Novel Drone Design Using an Optimization Software with 3D Model, Simulation, and Fabrication in Drone Systems Research. Drones, 6(4), p.97.

Oyesola, M., Mpofu, K., Daniyan, I. and Mathe, N., 2022. Design and simulation of a bearing housing aerospace component from titanium alloy (Ti6Al4V) for additive manufacturing.

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Brånäs, P. and Enderby, N., 2022. Automatic Creation of an Aircraft Structural Layout and Structural Analysis Model: A method for implementing design automation in an early conceptual design phase.

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