Image: Inlet shock waves at Mach 2

Original image(960 × 720 pixels, file size: 42 KB, MIME type: image/jpeg)

Description: Shock wave structure about a supersonic axisymmetric cone inlet. Left image shows unstarted flow. Right image shows started flow.
Title: Inlet shock waves at Mach 2
Credit: NASA document ID: C-1955-37520
Author: NASA Glenn Research Center
Usage Terms: Public domain
License: Public domain
Attribution Required?: No

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