Question: Load factor is defined as ___

Options

A : ratio of lift produced to the weight of aircraft

B : aerodynamic efficiency

C : thrust loading

D : power to weight ratio

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Airfoil Selection-1 more questions

An aircraft is cruising with lift of 150N. Find the....

An airfoil is subjected to the flow with temperature of....

Consider a NACA 2812 airfoil. It is operating with flow....

Find location of aerodynamic centre from leading edge if, chord....

If an airfoil has lift of 200 N at 10?....

Pitching moment co-efficient for an airfoil is given by ___

The cross-sectional shape of wing is called ___

The parameter marked by '?' in the diagram is ___^

We are using the airfoil in the aircraft as ___

Which of the following is not type of an airfoil?

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