Aeronautical Engineering Projects Titles For Essays

As part of the undergraduate studies the students in the faculty of aerospace engineering are required to participate in a yearlong design project of an aerospace system. In our project we were required to design an unmanned aerial vehicle (UAV) for instruction in flight tests and demonstration of flight test techniques. The tests will be based on the subjects studied in aerospace engineering such as stability and control, instruments, performance and propulsion.

We started off by reviewing all the main configuration aspects of UAV design and we made a list of a lot of possibilities for each aspect. We narrowed this list to 3 main configurations of UAVs that we thought were the best fitted for the design specification, using methods of conceptual design we evaluated the 3 configurations, and we found the configuration most suited for this project. We made a comprehensive survey of similar UAV in order to estimate the weight of the TeachAir UAV. We used design specification in order to define the main characteristic of the TeachAir UAV.

As part of the design process we placed high emphasis on aerodynamic issues including optimization of the airfoil, wing geometry, flaps, tail and ailerons and the drag coefficient was calculated. Another topic that we constricted on was propulsion and flight performance, this included finding the required power needed to meet design specifications and the engine and prop that can deliver them. After producing the propulsion system the flight characteristics and flight envelop were found. Using the characteristics we found we chose off the self components in order to comply with the design specification and planned the internal arrangement in order for our platform to be stable in all flight scenarios.

We then gave our attention to the design of the control system, performing stress analysis on critical parts and building a smaller scale model. During the design of the control system all of the control and stability were calculated, in addition, a simulation of six DOF was made and two controllers of pitch angle, and angle of attack due to elevator deflection were designed. Furthermore a thorough stress analysis of the forces and moments in the wing and in the main landing gear was made. Following the analysis the geometry and material of the wing beam and the landing gear were determined.

Besides theoretical work we also designed and built a small scale model which has the same aerodynamic properties as the TeachAir UAV. The process includes designing a CAD model and executing it in the faculty’s laboratory.

During this project we experienced the design process of a UAV aircraft including preliminary and specific sub system design, the entire process taught us a lot about the design aspects of aircraft and the considerations that need to be made during this process.

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Structures Project Ideas

1. The Efficiency of a Hybrid Flapping Wing Structure—A Theoretical Model Experimentally Verified

Fabrication and testing of  flexible flapping wing structure is carried out. read more

2. Nodal analysis of a control surface using FEM
3. Analysis of buffetting of aircraft wing using FEM
4. FEA Structural analysis of a high performance wing

These will be useful for you

Propulsion Project Ideas

Scramjet combustion chamber design

Design and analysis of rocket nozzle

 

1. Design and analysis of annular combustion chamber of a low bypass turbofan engine in a jet trainer aircraft

A low bypass turbofan engine for a jet trainer aircraft is designed and analysed using softwares. read more

2. Design and analysis of scramjet combustion chamber
3. Design and analysis of a high thrust parabolic nozzle using method of characteristics and CFD
4. Understanding the flow physics of Cascade blades
5. Design of cross flow injection system to enhance mixing in a supersonic flow

Quadcopter, MAV, UAV and Drone Project Ideas

1. The Efficiency of a Hybrid Flapping Wing Structure—A Theoretical Model Experimentally Verified

Fabrication and testing of  flexible flapping wing structure is carried out. read more

2.
3. Experimental evaluation of a MAV wing using subsonic wind tunnel
4. 35 quadcopter project ideas, titles and topics with pdf download

Design and modeling ideas, topics and titles for quadcopter projects, novel control ideas, topics and titles for quadcopter projects, Low cost / cheap quadcopter projects ideas, topics and titles and Project ideas, topics and titles for the application of Quadcopter are provided. read more

Design Project Ideas

1. Conceptual design for two seater single engine air plane
2. Design and development of one kg unmanned aerial vehicle
3. Design of a jet powered UAV

Where are Aeronautical Project center in Bangalore, karnataka, Chennai, Coimbatore Tamil Nadu, Hyderabad

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Titles, topics and Ideas for final year Mechanical and Aeronautical engineering student projects

For freshers, most of the technical interviews in aerospace domain are started with a question “What is your aeronautical project about“. Final year aeronautical project is your visiting card to the industry so this is the opportunity to show your capabilities as a fresher. Do you want to do a best aeronautical project which will place you above others during the job interview.

Other Aeronautical Ideas

Visit Aeronautical Projects Ideas & Topics

Title : Design of scramjet combustion chamber with intake and optimisation of injector geometry

What You get: Idea, Abstract (PDF), presentation for 0th review

Is Full Project Done : based on this Idea: Yes

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Title : Design of Mach 5 rocket nozzle using method of characteristics

What You get: Idea, Abstract (PDF), presentation for 0th review

Is Full Project Done : based on this Idea: Yes

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