Accession Number : AD0690165
Title : HEAT TRANSFER AND PRESSURE ON A SLENDER CYLINDER IN VISCOUS HYPERSONIC FLOW.
Descriptive Note : Rept. for Mar-Sep 68,
Corporate Author : AEROSPACE CORP EL SEGUNDO CALIF LAB OPERATIONS
Personal Author(s) : Varwig,Robert L.
Report Date : 30 APR 1969
Pagination or Media Count : 22
Abstract : Wall heat transfer and pressure were measured on a long, slender, cone-cylinder at positions far enough aft that transverse curvature effects were large. The tests were performed in the shock tunnel at M = 20 at Reynolds numbers of 0.8 to 4.0 x 10 to the 5th power based on free stream conditions and distance from the nose. The measurements were compared with hypersonic viscous interaction predictions. The resulting correlations showed that the strong interaction solution of the viscous interaction theory appeared to give accurate estimates of the heat transfer for large transverse curvature, regardless of shock strength. However, the pressures measured on the body were quite low, indicating a weak shock on the body. Hence, the present theory does not apply. Future pressure predictions will require consideration of finite shock strengths. (Author)
Descriptors : (*CYLINDRICAL BODIES, HYPERSONIC CHARACTERISTICS), (*HEAT TRANSFER, SLENDER BODIES), PRESSURE, VISCOSITY, REYNOLDS NUMBER, INTERACTIONS
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE