GD Pilot Physics MCQs
Solved MCQs of The Lifting Surface Theory for the job of GD Pilot physics MCQs
On the basis of loading, lifting surface problems are evaluated?
(A). True
(B). False
(C). Partially True
MCQ Answer: a
The achievements of powered flights are antedated by the loading of lifting surfaces.
(A). True
(B). False
(C). Partially True
MCQ Answer: a
Over a three-dimensional wing a mathematical model that predicts lift distribution is Prandtl lifting line theory?
(A). True
(B). False
(C). Partially True
MCQ Answer: a
On the platform downwash distribution is regular.
(A). True
(B). False
(C). Partially True
MCQ Answer: a
Smooth edge shapes are formed by the plan.
(A). True
(B). False
(C). Partially True
MCQ Answer: a
The analytically overall amount of lift is difficult to predict.
(A). True
(B). False
(C). Partially True
MCQ Answer: a
Normal velocity is related to subsonic lifting surface theory.
(A). True
(B). False
(C). Partially True
MCQ Answer: a
Along with the whole wingspan, the vortex loses the strength.
(A). False
(B). True
(C). Partially True
MCQ Answer: b
The lift over each wing segment corresponds.
(A). False
(B). True
(C). Partially True
MCQ Answer: a
The distribution of loading is represented by the sum of a finite number.
(A). True
(B). False
(C). Partially True
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