The supersonic airflow with expands at a deflection angle of 15 at a sharp corner (see picture).

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The supersonic airflow with

expands at a deflection angle of 15° at a sharp corner (see picture). Calculate and the angle of the front and rear Mach lines relative to the upstream flow direction. image text in transcribed

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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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Question Posted: Sep 20, 2024 06:01 AM

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The supersonic airflow with expands at a deflection angle of 15 at a sharp corner (see picture).

Question:

M = 1.5, Pi = 101325 Pa, T = 14.8C

Step by Step Answer:

Aerodynamics

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