What is the value of Cp at the forward surface in a biconvex airfoil? – McqOptions

MCQOPTIONS

1.	What is the value of Cp at the forward surface in a biconvex airfoil?
A.	Zero
B.	Positive
C.	Negative
D.	Infinite
Answer» C. Negative

Discussion

No Comment Found

Related MCQs

What is the source of wave drag exerted on the supersonic airfoil?
What happens to the coefficient of pressure in a supersonic flow for an increase in Mach number?
For supersonic flow, which differential equation is obtained for the linearized perturbation potential equation?
What is the lift coefficient over a flat plate at an angle of attack of 3 degrees in a supersonic flow at Mach 4?
Wave drag coefficient as derived from linearized theory is independent of the airfoil shape and thickness.
According to lineralized theory, what is the formula for coefficient of lift over the a flat plate in a supersonic flow?
The Cp value for supersonic airfoil surface which is inclined away from the freestream is positive.
What is the value of Cp at the forward surface in a biconvex airfoil?
Which of these equations is used for computing the lift and wave drag over a supersonic airfoil?