Question: Determine the corrections or otherwise of the following assertion [A] and reason [R]:^ Assertion [A]: Flying boats have higher values of empty weight fraction than that of the military aircraft.^ Reason[R]: Military aircraft has to be lighter in weight.

Options

A : Both [A] and [R] are true and [R] is the correct reason for [A]

B : Both [A] and [R] are true but [R] is not the correct reason for [A]

C : [A] is true but [R] is false

D : [A] is false but [R] is true

Click to view Correct Answer

Previous || Next

Conceptual Sketch Sizing - Empty-Weight Estimation more questions

Which of the following is the correct pair?

Which of the following pair is correct based on the....

Why do we use optimization after initial layout?

A military Aircraft should be designed to have __

Aircraft fuel weight does not include reserved fuel fraction.

The empty weight fraction of a jet transport with fixed....

Variable sweep wings have higher empty weight fraction than that....

A jet transport aircraft has fuel storage of 1200kg. It....

A prop-driven aircraft having fuel weight of 650kg. Now, aircraft....

According to FAA, general aviation aircraft requires reserved fuel in....

Aerodynamic Coefficients more Online Exam Quiz

Aerodynamics - Parasite (Zero-Lift) Drag and Drag due to Lift

Air Loads

Airfoil Selection-1

Airfoil Selection-3

Conceptual Design Process

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