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Interaction between the laminar boundary layer over a plane surface and an incident oblique shock wave, 1949 January 24
Collection Description & Creator Information
Consists of technical reports from the Department of Mechanical and Aerospace Engineering.
Access & Use
- Access Restrictions:
Collection is open for research use.
- Conditions for Reproduction and Use:
Single photocopies may be made for research purposes. For quotations that are fair use as defined under U. S. Copyright Law, no permission to cite or publish is required.
- Credit this material:
Interaction between the laminar boundary layer over a plane surface and an incident oblique shock wave; Department of Mechanical and Aerospace Engineering Reports, ENG007, Technical and Scientific Reports, Engineering Library, Princeton University Library
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