After passing through a normal shock wave, airflow is a. Subsonic. b. not changed in direction. c.

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After passing through a normal shock wave, airflow is

a. Subsonic.

b. not changed in direction.

c. heated up.

d. increased in pressure and density.

e. All of the above.

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Flight Theory And Aerodynamics

ISBN: 9781119772415

4th Edition

Authors: Joseph R. Badick; Brian A. Johnson

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