Measurements made for 5 sting configurations, including that of effectively removing sting for angles of attack from -- 2 to +20°, at constant Re of 1.4 million; results indicate that there is no feasible sting diameter for which interference on base pressures would be negligible; pertinence to atmosphere re-entry vehicles.
Effects of sting-support diameter on base pressures of elliptic cone at mach numbers from 0.60 to 1.40
NASA -- Tech Note
1961
30 pages
Report
English
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