List of top Aeronautical and Aerospace Engineering Questions on Airfoil Theory asked in TANCET

The lifting flow over circular cylinder is obtained by the combination of
Which of the following is usually measured as the angle between the line of 25% chord and a perpendicular to the root chord?
The schadowgraph flow visualization technique depends on
Flow separation is due to
What is the center pressure if the lift coefficient and lift curve slope of an aerofoil of percentage camber 0.6 are 1.02 and 2, respectively?
Aerodynamic center is defined as point on the airfoil at which
What is the Coefficient of pressure, where velocity at the surface of the cylinder is equal to free stream velocity?
The free stream Mach number for which the entire flow around the body is subsonic is called
When airfoil thickness decreases, the critical Mach number
What is the purpose of supercritical airfoil?