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A study of shock wave turbulent boundary layer interaction at M=3, 1953 July
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:
A study of shock wave turbulent boundary layer interaction at M=3; Department of Mechanical and Aerospace Engineering Reports, ENG007, Technical and Scientific Reports, Engineering Library, Princeton University Library
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