Here is the Top Aeronautical Engineering Project Titles and Abstracts for Final Year Engineering Students with Base Papers & Full Source Code.
List of Innovative Mechanical Engineering Projects Aerospace with Free PDF Downloads:
- Human-Powered Helicopter: A Program for Design and Construction
The various aspects of helicopter design and human-powered aircraft design were studied to present a program to build a human-powered helicopter (HPH) at the Naval Postgraduate School. The HPH will be designed to meet… - Modelling & implementation of Aerodynamic Zero-lift Drag into ADAPDT
The objective of this project work was to construct and implement an algorithm into the program ADAPDT to calculate the zero-lift drag profile for defined aircraft geometries. ADAPDT, short for AeroDynamic Analysis and Preliminary… - Analysis of Noise levels, Audio frequency and Fuel consumption with Propellers of type McCauley and MT on BAe Jetstream 32
This report describes a project conducted at Direktflyg in Borlänge, where the aim was to analyse the difference in noise level, audio frequency and fuel consumption between propellers of the older type McCauley and the newer… - VTOL Unmanned Aerial Helicopters – A Concept Study
This study deals with the development of a Conceptual Design Tool for unmanned helicopters, so called VTOL UAVs. The goal of the Design Tool is… - Aerodynamic Loads on External Stores – Saab 39 Gripen: Evaluation of CFD methods for estimating loads on external stores
External stores mounted on aircraft generate loads which need to be estimated before first takeoff. These loads can be measured in a wind tunnel but since the possible store configurations are basically endless, testing… - Simulation of Plume-Spacecraft Interaction
When the plume of a thruster impinges on spacecraft surfaces and instruments, the ow is either in the transitional or the free-molecular regime. The standard method to simulate the transitional regime is Direct Simulation… - Experiment of All Solid-State Electrochemical Sensor for Surface Chemistry Analysis for Adhesive Bonding
This project presents: 1) Literature review on adhesive bonding technologies in aviation industry including surface pretreatments (pre-preparation), surface quality assurance, and surface chemistry analysis methods… - Experimental and Numerical Investigations of a High Performance Co-Flow Jet Airfoil
The work reflected in this study includes a detailed study of co-flow jet (CFJ) technologies as they are applied to a typical thin airfoil, NACA 6415, at take-off and landing speeds. Numerical analysis and experimental testing were conducted… - 3D Fuel Tank Models for System Simulation
The purpose of the present master thesis is to optimize the current fuel tank simulations procedure for the next generation of JAS 39 Gripen ghters developed by SAAB AB. The current simulation process involves… - Design of a Hoverwing Aircraft
Wing-in-Ground effect aircraft is one that manages level flight near the surface of the Earth, making use of the aerodynamic interaction between the wings and the surface known as take advantage ground effect… - Theoretical Studies of Plasma Detachment in the Vasimr Magnetic Nozzle
In this thesis, theoretical studies are conducted to see whether plasma will detach from the magnetic field lines of the VASIMR thruster, and if so, at which location detachment takes place. A magnetic field similar… - Study of 3-Dimensional Co-Flow Jet Airplane and High-Rise Building Flow Using CFD Simulation
The purpose of this thesis is to design and study an aircraft which implements the Co-Flow Jet (CFJ) airfoil concept, as well as to study the CAARC standard highrise building. The design concept is verified mainly by the use of a Computational Fluid Dynamics… - Embedded Computer for Space Applications Suitable for Linux
This report briefly describes the special requirements for a computer board for use in space. In particular, component selection and ways of mitigating the soft and hard errors are discussed. Furthermore, one implementation… - Simulation Method Development of Ultra Thick Laminates:: with Cohesive Zone Method and Empirical Arcan Tests
To reduce the product life cost of aircrafts, the conversion of major load bearing components from aluminium to carbon fibre reinforced plastics have been proposed. Large load bearing components require significantly thicker composite… - Interval Based Integer Ambiguity Resolution Using Multiple Antennas: Applied to airplane attitude determination
Finding the correct integers is the key to high precision range measurements. This has been an issue of investigation since the early 1980’s and many different techniques have been developed, none of them can guarantee… - Wingbox Mass Prediction considering Quasi-Static Nonlinear Aeroelasticity
Nonplanar wing configurations promise a significant improvement of aerodynamic efficiency and are therefore currently investigated for future aircraft configurations. A reliable mass prediction for a new wing configuration… - Injector design and test for a high power electrodeless plasma thruster
The HPEP (High Performance Electric Propulsion) thruster is expected to be the outcome of an innovative project initiated by the Swedish Space Corporation. It combines the concept of a 10 kW electrodeless plasma thruster… - Design of a Four Rotor Hovering Vehicle
Potential applications of autonomous vehicles range from unmanned surveillance to search and rescue applications dangerous to human beings. Vehicles specifically designed for hover flight have their own possible applications… - Analysis of Metal to Composite Adhesive Joins in Space Applications
Within the European space program, a new upper stage engine (Vinci) for the Ariane 5 launcher is being developed, and the Volvo Aero Corporation (VAC) is contributing with turbines for the fuel turbo pumps. This study investigates… - An Explication of Airfoil Section Bending-Torsion Flutter
This study examines the dynamic instability known as flutter using a two-degree-of-freedom airfoil section model in both quasi-steady and unsteady flow. It explains the fundamental forces and moments involved in the bending-torsion… - Validation and Integration of a Rubber Engine Model Into an MDO Environment
Multidisciplinary design optimization (MDO) is a technique that has found use in the field of aerospace engineering for aircraft design. It uses optimization to simultaneously solve design problems with several disciplines… - Augmented Reality for Space Applications
Future space exploration will inevitably require astronauts to have a higher degree of autonomy in decision-making and contingency identification and resolution. Space robotics will eventually become a major aspect of this new challenge… - Value Stream Mapping for an Office Environment
To be more flexible and efficient in a process, lean and all of its methods can be used to improve your workplace. This study was carried out by two aeronautical engineering students from Malardalens University Vasteras… - Assembly of a UAV (Unmanned Aerial Vehicle): hardware design of a UAV
This project is dedicated to assemble the hardware system of a UAV (Unmanned Aerial Vehicle) in order to prepare the platform for an autonomous flight in the air for a given path through the pre-programmed check points… - Continuing Airworthiness Management Exposition: For Priority Aero Maintenance
The economic crisis has affected the airline industry as much as it has affected all other industries in the world. The small airlines and maintenance organisations must find new opportunities and options in order to survive… - West Helicopter AB Aircraft Technical Status Report
Westhelicopter INC. has an aviation workshop providing qualified helicopter maintenance in accordance with PART-145. Maintenance and administrative base is situated in Luleå at Kallax airport. The types that Westhelicopter… - Development and Documentation of Process and Routines for Continuous Air worthiness Management Organisation
This report provides a description of a work in aeronautical engineering that was carried out at Patria Helicopters AB. Patria have been responsible for the preservation of a Eurocopter EC135 since May of last year due to the fact… - Robust Repair Methods of Primary Structures in Composite
A request of material change when performing repairs on composite parts of SAABs JAS 39 Gripen has lead to the initiation of this project. The aim is to create a quicker and more robust repair method… - Design and Construction of a Passenger Hovercraft
The purpose of our senior design project is to construct a functioning hovercraft designed through fundamental principles. Through this design project, we explore the process of engineering from initial design to product construction… - MD-80 Engine Change Kit
This report’s aim is to verify if it is possible, and if so, by how much SAS Component could increase the threshold values of all incoming components belonging to an MD-80 Engine Change Kit. How would this raise in the components threshold lower SAS Component’s… - Analysis of Casting Process for Complex Electronic Unit
Most aircraft component are currently being manufactured by machining, forging, welding and also assembling such parts. However, the possibilities of cutting cost from a single component has brought about a growing trend… - MSC Adams modelling of mechanical system in A400M Crew Entrance Door
Saab Aerostructures has developed the Crew Entrance Door (CED) for Airbus A400M. Airbus has decided some different load cases for which the Crew Entrance Door must be built to withstand without something breaking down…
>> More Aeronautical Avionics Space Projects For Mech Students
>> More Aeronautical Projects For Engineering Students