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An investigation of the flow around slender delta wings with leading edge separation, 1960 May
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:
An investigation of the flow around slender delta wings with leading edge separation; Department of Mechanical and Aerospace Engineering Reports, ENG007, Technical and Scientific Reports, Engineering Library, Princeton University Library
- Engineering LibraryEngineering LibraryFriend Center for Engineering EducationPrinceton, NJ 08540, USA(609) firstname.lastname@example.org