GATE_AE_2027_MOCK_04_Q16
GATE 2027 Aerospace Engineering All-India Master Mock 04 (Aerospace Structures, Thin-Walled Beams & Aeroelasticity)
MCQ · 1 Mark
Aerodynamics & Fluid Mechanics • Basic Fluid Mechanics • Continuity, Momentum & Energy Equations
In steady incompressible inviscid flow along a streamline, the sum of static pressure and dynamic pressure is constant according to:
(A) Bernoulli's theorem
(B) Fourier's law
(C) Fick's law
(D) Hooke's law
Answer Key:
A
Step-by-Step Verified Solution
### Solution: p + 0.5 * rho * V^2 = p_0 = constant along a streamline in frictionless incompressible flow is Bernoulli's theorem. Correct: A.