References:
• Pilot Operating Handbook e.g. http://www.faaflyingclub.com/N75190-POH.pdf ,
• aerofoil data NACA 65-415 (PA 28 Archer/Warrior) http://brandongilyard.weebly.com/uploads/2/1/7/7/21776120/aerodynamics_final_project.pdf
• calculation specifics http://www.diva-portal.org/smash/get/diva2:752136/fulltext01.pdf ,
• www in general,
• textbooks listed and used for AVS 209 (Syllabus).
Results to be documented in a written report and basis of assessment!
Research paper
Discuss in detail:
1. Aerodynamic design parameters:
A. Aerofoil,
B. wing geometry,
C. wing-dihedral,
D. horizontal tail geometry vs. location (arm)
2. Study the force couples Lift/Weight and Drag/Thrust and calculate representative values for
a. Cruise flight at 1.000 ft and 10.000 ft MSL ISA
b. Consider a max forward and a max aft CG position and calculate the
required tail-plane force to ensure steady state flight
3. Same as question in number 2 part a. for best rate of climb and best glide angle for one common CG position
PRIORITIZE SOLVING THE QUESTION COMPLEX CALCULATIONS.
SHOW THE SOLUTIONS. STEP BY STEP