Configuration Layout - Aerodynamic Considerations-2 Online Exam Quiz

Configuration Layout - Aerodynamic Considerations-2 GK Quiz. Question and Answers related to Configuration Layout - Aerodynamic Considerations-2. MCQ (Multiple Choice Questions with answers about Configuration Layout - Aerodynamic Considerations-2

Area rule can be used for high speed aircraft only.

Options

A : TRUE

B : FALSE

C : -

D : -

View Answer

Drag divergence Mach number will increase by using ___

Options

A : area rule

B : increment in total volume

C : increase in drag

D : drag increment at maximum area

View Answer

Interaction of components will not affect aerodynamic design of fuselage.

Options

A : TRUE

B : FALSE

C : -

D : -

View Answer

Process of determining the take-off gross weight and required fuel weight is called as __

Options

A : aircraft sizing

B : aircraft Lofting

C : aircraft drafting

D : aircraft drawing

View Answer

Supersonic wave drag can be reduced by using __

Options

A : area rule

B : drag ruling

C : lift augmentation

D : drag augmentation

View Answer

Vortex generator is used to __

Options

A : reattach separated flow

B : increase volume

C : increase surface area

D : separate flow

View Answer

We can provide sizing based on new design only.

Options

A : TRUE

B : FALSE

C : -

D : -

View Answer

Aerodynamic Coefficients more Online Exam Quiz

Conceptual Sketch Sizing - Fuel-Fraction Estimation-1

Conceptual Sketch Sizing - Fuel-Fraction Estimation-2

Conceptual Sketch Sizing - Takeoff-Weight Buildup

Conceptual Sketch Sizing - Takeoff-Weight Calculation

Configuration Layout - Aerodynamic Considerations-1

Configuration Layout - Conic Fuselage Development

Configuration Layout - Conic Lofting

Configuration Layout - Crashworthiness Considerations

Configuration Layout - Maintainability Considerations

Configuration Layout - Producibility Considerations