Task: Principle Review on the aerodynamic design of a Piper PA 28 Archer
aerofoil data NACA 65-415 (PA 28 Archer/Warrior)
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 page 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 geometryvs. 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
Indicate any assumptions used if necessary to substitute for lack of data.