Which is not true for continuity equation of normal shock? – McqOptions

MCQOPTIONS

1.	Which is not true for continuity equation of normal shock?
A.	<sub>1</sub>u<sub>1</sub>A<sub>1</sub>= <sub>2</sub>u<sub>2</sub>A<sub>2</sub>
B.	<sub>1</sub>u<sub>1</sub>= <sub>2</sub>u<sub>2</sub>
C.	Steady flow
D.	No viscosity
Answer» C. Steady flow

Discussion

No Comment Found

Related MCQs

Mach number is a measure of the directed motion of the gas compared with the random thermal motion of the molecules.
The isentropic compressibility, in terms of speed of sound in any medium is given by ________
The speed of sound in any medium is a function of_____
The fundamental expression for the speed of sound in a gas is not given by which of the following equations?
The equation a=- ( frac {da}{d rho } ) where a is the speed of sound in the medium is the mathematical expression derived for the sound waves, which are _________
The most important quantity that dominates the physical properties of compressible flow is _______
The incorrect equation for the normal shock equation is_______
Which is not true for continuity equation of normal shock?
Which of these is incorrect for the normal shock wave analysis?
A shock wave that is normal to the upstream flow is a rare case.