Question: Determine the corrections or otherwise of the following assertion [A] and reason [R]:^ Assertion [A]: In general, wing twist should not be more than 6?.^ Reason[R]: Wing twist is used to improve stall properties at tip.
Options
A : Both [A] and [R] are true and [R] is the correct reason for [A]
B : Both [A] and [R] are true but [R] is not the correct reason for [A]
C : [A] is true but [R] is false
D : [A] is false but [R] is true
Wing Geometry-2 more questions
Wing aspect ratio is defined as ___
Wing planform is affected by ___
An aircraft with elliptic wing planform has parasite drag coefficient....
An aircraft with elliptic wing planform has parasite drag coefficient....
Canard pusher aircraft uses wing sweep to change location of....
Excessive dihedral can produce ___
If root chord is 2m and tip chord is 0.9m....
Let's consider an aircraft has statistically determined aspect ratio of....
Only convergent section will be used for supersonic speeds.
Performance of engine can be controlled by nozzle.
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