Question: Short and fat fuselage will have ___

Options

A : lower tail arm

B : higher tail arm

C : higher fineness ratio

D : higher wetted area

Click to view Correct Answer

Previous || Next

Configuration Layout - Aerodynamic Considerations-1 more questions

To reduce fuselage wetted area we can ___

Total take-off gross weight depends on ___

Which of the following is correct?

A fuselage is designed as show in below diagram. If....

Determine the corrections or otherwise of the following assertion [A]....

What is the disadvantage of short and fat fuselage?

Area rule can be used for high speed aircraft only.

Drag divergence Mach number will increase by using ___

Interaction of components will not affect aerodynamic design of fuselage.

Process of determining the take-off gross weight and required fuel....

Aerodynamic Coefficients more Online Exam Quiz

Conceptual Sketch Sizing - Empty-Weight Estimation

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-2

Configuration Layout - Conic Fuselage Development

Configuration Layout - Conic Lofting

Configuration Layout - Crashworthiness Considerations

Configuration Layout - Maintainability Considerations