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Preliminary results from a free-flight investigation of boundary-layer transition and heat transfer on a highly polished 8-inch-diameter hemisphere-cylinder at Mach numbers up to 3 and Reynolds numbers based on a length of 1 foot up to 17.7 x 10(exp
- Publication Year :
- 1957
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1957.
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Publication Type :
- Report
- Accession number :
- edsnas.19930089771
- Document Type :
- Report