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Investigation of flow characteristics over missile bodies at supersonic speeds
- Publication Year :
- 1979
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1979.
-
Abstract
- Three missile body shapes tested at Mach numbers of 1.50, 2.16, and 2.86 with angles of attack up to 30 degrees are described. The flow characteristics for each body shape are examined. The measured aerodynamic forces and moments are presented. The use of flow visualization techniques are described and the results such as vortex effects are discussed.
- Subjects :
- Aerodynamics
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Notes :
- RTOP 505-43-23-02
- Publication Type :
- Report
- Accession number :
- edsnas.19800004746
- Document Type :
- Report