Empennage sizing with the tail volume complemented with a method for dorsal fin layout
Design Summary
SOLVED: Consider an airplane with the following characteristics Horizontal tail volume ratio:0.38 Tail efficiency:1 Lift slope of the wing airfoil/:0.097 per degree Chord:1m Location of center of gravity of aircraft:0.31 m Location
Surjeet Yadav
D & C PDR #1 AAE451 – Team 3 November 4, ppt video online download