Comprehensive MCQs in physics
which of the following are the flows in which all flow parameters are the function of ‘x’ ________
(A). 3D flow
(B). 2D flow
(C). Quasi 1D flow
(D). Quasi 2D flow
(E). None of these
MCQ Answer: c
The density is ________ in incompressible flow
(A). 0
(B). constant
(C). varies from point to point
(D). negligible
(E). None of these
MCQ Answer: b
What is it called when the area is minimum in a section, in a wind tunnel?
(A). exit
(B). nozzle
(C). inlet
(D). throat
(E). None of these
MCQ Answer: d
What is the pressure at the throat in a venturi duct?
(A). lower than ambient pressure
(B). equal to ambient pressure
(C). greater than ambient pressure
(D). 0
(E). None of these
MCQ Answer: a
In an automobile engine, the carburetor makes use of ___
(A). venturi duct
(B). convergent duct
(C). divergent duct
(D). wind tunnel
(E). None of these
MCQ Answer: a
By using venturi which parameter can be measured?
(A). temperature
(B). velocity
(C). volume
(D). density
(E). None of these
MCQ Answer: a
The incompressible flow application in a duct is?
(A). High-speed wind tunnel
(B). Low-speed wind tunnel
(C). Flow in air
(D). Cannot be said
(E). None of these
MCQ Answer: b
Venturi duct is same as the open-circuit wind tunnel ____
(A). True
(B). False
(E). None of these
MCQ Answer: a
what is that section called where the area further decreases from A2 to A3 Inside a wind tunnel?
(A). Converging section
(B). Divergent section
(C). Throat section
(D). Nozzle
(E). None of these
MCQ Answer: b
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