GATE_AE_2027_MOCK_02_Q16
GATE 2027 Aerospace Engineering All-India Master Mock 02 (Compressible Aerodynamics & High-Speed Propulsion)
MCQ · 1 Mark
Aerodynamics & Fluid Mechanics • Basic Fluid Mechanics • Incompressible Potential Flow & Vorticity
For an irrotational, incompressible planar flow, the velocity components $(u, v)$ in terms of velocity potential $\Phi$ are related to stream function $\psi$ by:
(A) $u = \frac{\partial \Phi}{\partial x} = \frac{\partial \psi}{\partial y}$, $v = \frac{\partial \Phi}{\partial y} = -\frac{\partial \psi}{\partial x}$
(B) $u = \frac{\partial \Phi}{\partial y} = \frac{\partial \psi}{\partial x}$, $v = -\frac{\partial \Phi}{\partial x} = \frac{\partial \psi}{\partial y}$
(C) $u = -\frac{\partial \Phi}{\partial x} = \frac{\partial \psi}{\partial y}$, $v = -\frac{\partial \Phi}{\partial y} = -\frac{\partial \psi}{\partial x}$
(D) $u = \frac{\partial \psi}{\partial x}$, $v = \frac{\partial \psi}{\partial y}$
Answer Key:
A
Step-by-Step Verified Solution
### Solution: By Cauchy-Riemann conditions for potential flow: $u = \frac{\partial \Phi}{\partial x} = \frac{\partial \psi}{\partial y}$ and $v = \frac{\partial \Phi}{\partial y} = -\frac{\partial \psi}{\partial x}$. Correct: A.