Project translated automatically.
Log in
or
register,
to view the original
Objective of the work:
To develop a preliminary layout of a fixed-wing UAV and perform basic aerodynamic calculations to assess flight characteristics.
Scope of work:
Development of the overall layout of the UAV:
sketch diagram of the aircraft (fuselage, wing, tail, engine placement);
determination of the main geometric parameters (wingspan, wing area, aspect ratio, sweep angle, etc.).
Aerodynamic calculation:
assessment of aerodynamic characteristics (CL, CD, CM);
stability and control analysis;
performing calculations using XFLR5 (or equivalent software).
Control surfaces calculation:
determination of the areas and geometry of the elevators, ailerons, and rudders;
checking their effectiveness in the working speed range.
Results of the work:
description of the layout and accepted technical solutions;
2D diagrams or sketches of the layout;
XFLR5 project file(s) or report with calculation results;
recommendations for further design.
Input data:
Provided by the client after agreement.
