Physics MCQs pdf download
At the downstream thin sheet of intense vorticity is unstable?
(A). True
(B). False
(C). Partially True
MCQ Answer: a
The density of the inviscid incompressible fluid is constant?
(A). False
(B). True
(C). Partially True
MCQ Answer: a
‘C’ indicates a dyed circuit, composed of the same fluid particles?
(A). False
(B). True
(C). Partially True
MCQ Answer: b
To weaker conditions, kelvin established his result subject?
(A). True
(B). False
(C). Partially True
MCQ Answer: a
The dyed circuit is not required for kelvin circulation?
(A). True
(B). False
(C). Partially True
MCQ Answer: a
Around the C, the circulation is constant?
(A). True
(B). False
(C). Partially True
MCQ Answer: a
To generate the lift on an airfoil the starting vortex is necessary?
(A). True
(B). False
(C). Partially True
MCQ Answer: a
Around the closed-circuit, the circulation is zero?
(A). True
(B). False
(C). Partially True
MCQ Answer: a
Around the airfoil what is the circulation?
(A). Positive
(B). Negative
(C). Constant
(D). Slightly varies
MCQ Answer: b
Initially, the fluid is in irrotational motion?
(A). True
(B). False
(C). Partially True
MCQ Answer: a
Around a closed curve, the time rate of change of circulation is zero?
(A). True
(B). False
(C). Partially True
MCQ Answer: a
Physics MCQs pdf download
Aerodynamics MCQs
- Infinitesimal Fluid Element
- Kelvin’s Circulation Theorem and the Starting Vortex
- Laminar Flow MCQs
- Lifting Flow over Cylinder MCQs
- FRCR Physics MCQs
- Non-lifting Flow over Arbitrary Bodies MCQs
- Pathlines, Streamlines, Streaklines Physics MCQs
- Pitot Tube MCQs Physics
- Classical Lifting-Line Theory MCQs
- Doublet Flow MCQs
- Flow in Duct
- Continuity Equation MCQs
- Cambered Airfoil MCQs
- Kutta Condition MCQs
- Lifting Surface Theory MCQs
- Symmetric Airfoil MCQs
- The Vortex Filament, Biot-Savart Law, Helmholtz Theorem MCQs
- IAF Physics MCQs
- Viscous Flow MCQs
- Uniform and Turbulent Flow MCQs
- Three Dimensional Source and Three Dimensional Doublet MCQs
- Vortex Sheet MCQs
- Pressure Coefficient MCQs
- Source Flow MCQs
- Angular Velocity, Strain and Vorticity MCQs
- Bernoulli’s Equation MCQs
- MCQs on Circulation
- Finite Control Volume Approach MCQs
- Flow over Sphere MCQs
- Airfoil Characteristics MCQs
- Downwash and Induced Drag MCQs
- Aerodynamics MCQs
- Airfoil Nomenclature MCQs