Subsonic Speed

51 books
Response of high subsonic jet to nonaxisymmetric disturbancesAlvin Bayliss

Response of high subsonic jet to nonaxisymmetric disturbances

Alvin Bayliss

1997No page data
Design of supersonic transport flap systems for thrust recovery at subsonic speedsMichael J. Mann

Design of supersonic transport flap systems for thrust recovery at subsonic speeds

Michael J. Mann

1999No page data
Noise impact of advanced high lift systemsKevin R. Elmer

Noise impact of advanced high lift systems

Kevin R. Elmer

1995No page data
Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speedsUnknown Author

Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds

Unknown Author

2001No page data
Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speedsUnknown Author

Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds

Unknown Author

2001No page data
Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplaneDennis O. Allison

Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane

Dennis O. Allison

1995No page data
Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speedsJohn E. Lamar

Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds

John E. Lamar

2001No page data
Study of potential aerodynamic benefits from spanwise blowing at wingtipRaymond E. Mineck

Study of potential aerodynamic benefits from spanwise blowing at wingtip

Raymond E. Mineck

1995No page data
Ultra-high bypass ratio jet noiseLow, John, K. C.

Ultra-high bypass ratio jet noise

Low, John, K. C.

1994No page data
Pressure distributions from subsonic tests of a NACA 0012 semispan wing modelZachary T. Applin

Pressure distributions from subsonic tests of a NACA 0012 semispan wing model

Zachary T. Applin

1995No page data
Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attackKevin R. Walsh

Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack

Kevin R. Walsh

1997No page data
Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planformsKevin J. Kjerstad

Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms

Kevin J. Kjerstad

1999No page data
Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attackUnknown Author

Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack

Unknown Author

1997No page data
Low-speed wind tunnel tests of two waverider configuration modelsRobert J. Pegg

Low-speed wind tunnel tests of two waverider configuration models

Robert J. Pegg

1995No page data
Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic FacilityPeter F. Jacobs
⏱ 1h 7m

Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility

Peter F. Jacobs

198967 pp.
Subsonic dynamics of stardust sample return capsuleR. A. Mitcheltree

Subsonic dynamics of stardust sample return capsule

R. A. Mitcheltree

1997No page data
Static performance of six innovative thrust reverser concepts for subsonic transport applicationsScott C. Asbury

Static performance of six innovative thrust reverser concepts for subsonic transport applications

Scott C. Asbury

2000No page data
Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraftUnknown Author

Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft

Unknown Author

1999No page data
Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number rangesJulio Chu

Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges

Julio Chu

1996No page data
Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraftUnknown Author

Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft

Unknown Author

1999No page data
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