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Castner, Raymond S.
ID:
1392322
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Castner, Raymond S.
Castner Raymond S.
Castner Raymond S
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Background pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel
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Exhaust nozzle plume and shock wave interaction
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Exhaust nozzle plume effects on sonic boom test results for isolated nozzles
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Exhaust nozzle plume effects on sonic boom test results for vectored nozzles
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Slot nozzle effects for reduced sonic boom on a generic supersonic wing section
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Supersonic inlet test for a quiet supersonic transport technology demonstrator in the NASA Glenn 8-by 6-foot supersonic wind tunnel
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Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles
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