Physics MCQs for entry test ECAT
In an unbroken stream, the flow of jet of oil can be attributed?
(A). Capillarity
(B). Surface tension
(C). Temperature
(D). Density
(E). None of these
MCQ Answer: b
Newtonian’s fluid example is?
(A). Water
(B). Plastic
(C). Colloids
(D). Gel
(E). None of these
MCQ Answer: a
The point on the body where the resultant forces act is called enter of pressure.
(A). True
(B). False
(E). None of these
MCQ Answer: a
Due to which principle the aircraft flies in the atmosphere?
(A). Archimedes principle
(B). Bernoulli’s principle
(C). Gravitational force
(D). Newton’s law of viscosity
(E). None of these
MCQ Answer: b
What is V, In an equation? V=1/ v*D (v)/Dt ___
(A). change in velocity
(B). divergence of velocity
(C). volume
(D). velocity as a function of time
(E). None of these
MCQ Answer: b
Under which flow similarity, scale, volume, and length fall?
(A). Geometric Similarity
(B). Kinematic Similarity
(C). Dynamic Similarity
(D). Dimensionless number
(E). None of these
MCQ Answer: a
The shock wave is formed in?
(A). subsonic flow
(B). transonic flow
(C). supersonic flow
(D). incompressible flow
(E). None of these
MCQ Answer: c
For a fluid which of the following is a suitable flow model?
(A). Finite control volume approach
(B). Infinitesimal fluid element approach
(C). Molecular approach
(D). All three models can be applied based on the requirement
(E). None of these
MCQ Answer: d
Under which flow similarity, the force of inertia falls?
(A). Geometric Similarity
(B). Kinematic Similarity
(C). Dynamic Similarity
(D). Dimensionless number
(E). None of these
MCQ Answer: c
Which of the following is the ratio of Reynold’s number?
(A). Inertia force to viscous force
(B). Viscous force to inertia force
(C). Inertia force to gravity force
(D). Pressure force to inertia force
(E). None of these
MCQ Answer: a
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