Why speed of sound is always used as reference point; examination of effects of compressability; results from tests on conventional airfoil section, made in high speed tunnel; new airfoil sections, which will not "shock stall" until much higher speed than M equal to .6 is reached, must be developed.
What happens at high speeds?
Can Aviation
Canadian Aviation ; 19 , n 2
1946
Article (Journal)
English
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