Tutorial Sheet 2 Flashcards
(2 cards)
1
Q
Aspect Ratio in terms of wing area and chord
A
AR=S/c^2
2
Q
Determining trim lift coefficient?
A
AER324 - Aircraft Dynamics and Control > Tutorial Sheet 2 > Flashcards
Aspect Ratio in terms of wing area and chord
AR=S/c^2
Determining trim lift coefficient?
AER324 - Aircraft Dynamics and Control (15 decks)