A New Conceptual Design Tool for General Aviation Aircraft (FLEX) : A user-friendly computer implementation of classical design methods
This report is a part of a thesis work at the division of Fluid and Mechatronic Systems(Flumes) at Linkoping University. The aim of this thesis is to build a robust, advanced, simple, easy to maintain, easy to develop and user-friendly program for the general aviation aircraft conceptual design. The...
Main Author: | Salaymeh, Ammar |
---|---|
Format: | Others |
Language: | English |
Published: |
Linköpings universitet, Fluida och mekatroniska system
2018
|
Subjects: | |
Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-150518 |
Similar Items
-
On Subscale Flight Testing : Applications in Aircraft Conceptual Design
by: Sobron, Alejandro
Published: (2018) -
Creation and Validation of Early Stage Conceptual Design Methodology for Blended WingBody Aircraft
by: Lejon, Alexander
Published: (2019) -
Implications of Designing Unstable Aircraft from a Flight Control Perspective
by: Johansson, Emil
Published: (2018) -
Conceptual Design and Analysis of an Unmanned Autonomous Expendable Air Vehicle
by: Huzelius, Alicia, et al.
Published: (2018) -
Conceptual Design of a Small Size Unmanned Air Vehicle : Part A: Aerodynamic Performance and Structural Design
by: Pellnäs, Adrian, et al.
Published: (2021)