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Recent studies of factors affecting high lift- drag ratios at M equals 19 in helium.
- Publication Year :
- 1967
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1967.
-
Abstract
- Aerodynamic performance characteristics of three entry vehicles designed for maximum L/D ratio of three and two at Mach 19 and Reynolds number 3,200,000 tested in 22-inch Langley helium tunnel
- Subjects :
- Aerodynamics
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Publication Type :
- Report
- Accession number :
- edsnas.19670039710
- Document Type :
- Report