Question: At same value of maximum lift AOA, lift coefficient of Cambered wing is ___
Options
A : higher than uncambered wing
B : lower than uncambered wing
C : same as cambered airfoil always
D : not dependent on camber
Aerodynamic Forces more questions
Cambered wing has minimum drag coefficient of 0.05 and constant....
For a symmetrical airfoil drag coefficient at zero lift is....
___ is one of the sources of drag.
A 2D airfoil is operating at 0.6M. Find the approximate....
Aerodynamic forces are generated due to __
Consider an incompressible flow. If static pressure increases then, the....
Drag which is produced due to lift is called?
For an incompressible flow, if local area velocity decreases then,....
For ideal flow, total pressure along streamline will be ___
If I want to design an aircraft which primary flies....
Aerodynamic Coefficients more Online Exam Quiz
Testing Aircraft Materials - Inspection Methods-1
Testing Aircraft Materials - Inspection Methods-2
Wrought Aluminium and it's Alloys
Aerodynamics - Parasite (Zero-Lift) Drag and Drag due to Lift