Question: Consider a NACA 2812 airfoil. It is operating with flow velocity of 900m/s with chord of 1m. What should be the maximum thickness of this airfoil?
Options
A : 0.12m
B : 0.21m
C : 0.9m
D : 28.12m
Click to view Correct Answer
Airfoil Selection-1 more questions
Aerofoil affects the performance parameters of aircraft.
Airfoil is a streamline shape.
An aerofoil is operating with flow velocity of 100m/s. Aerofoil....
An aircraft is cruising with lift of 150N. Find the....
An airfoil is subjected to the flow with temperature of....
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 ___
Aerodynamic Coefficients more Online Exam Quiz
Aerodynamics - Parasite (Zero-Lift) Drag and Drag due to Lift
Conceptual Sketch Sizing - Empty-Weight Estimation