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File:2D-wedge-oblique-shock-expansion-Mach 2-Penn-State-Gas-Dynamics-Lab.jpg

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English: This schlieren image depicts 2-D supersonic airflow over a wedge at Mach 2. Oblique shock waves, followed by Prandtl-Meyer expansion fans, are revealed. This image was taken in the supersonic wind tunnel of the Penn State University Gas Dynamics Laboratory.
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Author Settles1

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current19:19, 4 May 2015Thumbnail for version as of 19:19, 4 May 2015627 × 667 (291 KB)Settles1 (talk | contribs)User created page with UploadWizard

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