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
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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