Aerospace Engineering > GATE 2010 > Longitudinal Stability
The Irim curves of an aircraft are of the form Cm,...=(0.05-0.2δ)-0.1Ct where the elevator
deflection angle, δr, is in radians. The static margin of the aircraft is:
deflection angle, δr, is in radians. The static margin of the aircraft is:
Explanation
Correct : c
Similar Questions
What is the worst-case time complexity of insertion in an AVL tree?
Which operations on a binary search tree have O(h) complexity?
Compare search complexities of sorted array vs balanced BST.