Compressors, Gas Dynamics and Gas Turbines - Data Intensity 3 Multiple Questions and Answers.




16.Slope between lift coefficient and angle of attack in a line is __________
A. 90 degree
B. 180 degree
C. 360 degree
D. 60 degree

17.Center of pressure lies exactly in ________ of the chord from the leading edge in a symmetrical air foil.
A. one quarter
B. half
C. three fourth
D. none of the mentioned

18.Aerodynamic center lies exactly at ______ on the chord from leading edge in cambered air foil.
A. half
B. one quarter
C. three fourth
D. none of the mentioned

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