Search Results - Castner, Raymond
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1
Slot nozzle effects for reduced sonic boom on a generic supersonic wing section by Castner, Raymond S.
Published 2010Call Number: Loading…Online Access
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Government Document Electronic Conference Proceeding eBook -
2
Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles by Castner, Raymond S.
Published 2010Call Number: Loading…Online Access
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Government Document Electronic Conference Proceeding eBook -
3
Exhaust nozzle plume effects on sonic boom test results for vectored nozzles by Castner, Raymond S.
Published 2012Call Number: Loading…Online Access
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Government Document Electronic Conference Proceeding eBook -
4
Exhaust nozzle plume effects on sonic boom test results for isolated nozzles by Castner, Raymond S.
Published 2011Call Number: Loading…Online Access
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Government Document Electronic Conference Proceeding eBook -
5
Exhaust plume effects on sonic boom for a delta wing and a swept wing-body model by Castner, Raymond
Published 2012Call Number: Loading…Online Access
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Government Document Electronic Conference Proceeding eBook -
6
The nozzle acoustic test rig an acoustic and aerodynamic free-jet facility / by Castner, Raymond S.
Published 1994Call Number: Loading…
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7
Background pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel / by Castner, Raymond S.
Published 2013Call Number: Loading…Online Access
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Government Document eBook -
8
Design and checkout of a high speed research nozzle evaluation rig by Castner, Raymond S.
Published 1997Call Number: Loading…
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9
Supersonic inlet test for a quiet supersonic transport technology demonstrator in the NASA Glenn 8-by 6-foot supersonic wind tunnel / by Castner, Raymond S., Simerly, Stephanie, Rankin, Michael
Published 2018Call Number: Loading…Online Access
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10
Exhaust nozzle plume and shock wave interaction / by Castner, Raymond S., Elmiligui, Alaa, Cliff, Susan
Published 2013Call Number: Loading…Online Access
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11
Numerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design / by Friedlander, David J., Heath, Christopher M., Castner, Raymond S.
Published 2018Call Number: Loading…Online Access
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Government Document eBook -
12
A study of highly underexpanded supersonic jets in subsonic crossflow / by Schindler, Ryan D., Castner, Raymond S., Zaman, B. M. Q.
Published 2022Call Number: Loading…Online Access
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Related Subjects
Sonic booms
Computational fluid dynamics
Exhaust nozzles
Supersonic aircraft
Plumes
Supersonic wind tunnels
Elastic waves
Exhaust gases
Nozzle flow
Pressure distribution
Pressure ratio
Aerodynamic configurations
Aerodynamic stability
Aircraft control
Airplanes
Body-wing configurations
Computerized simulation
Convergent-divergent nozzles
Design analysis
Evaluation
F-15 aircraft
Grid refinement (mathematics)
High aspect ratio
High speed
Low cost
Mach number
Motors
Nozzle geometry
Nozzles
Pressure sensors