Solved MCQs of The Lifting Surface Theory for the job of GD Pilot p*hysics* 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

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