Question: Wave drag is produced due to __
Options
A : shock wave formation
B : incompressible flow
C : fluid is not compressible
D : flow separation of incompressible flow
Aerodynamic Forces more questions
Increment in the skin friction drag due to prop-wash is....
Induced drag of the airfoil is ___
Skin friction drag is defined as ___
The change in local air flow velocity will produce small....
The location of separation point will depend on __
A subsonic aircraft has unswept wing which has maximum lift....
A subsonic aircraft wing has aspect ratio of 8. Now....
A supersonic 2D airfoil has Mach number of 1.5. Find....
If an airfoil is designed to provide lift curve slope....
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