Add to ORKGThe YF-16 and F-16 developmental wind tunnel test program was reviewed and all force data pertinent to the design of forebody and nose strakes extracted. A complete set of these data is presented without analysis
The method described in this report is intended to present an overview of a process developed to ext...
For a body of revolution with afterbody side strakes, an experimental investigation was conducted in...
A systematic water-tunnel study was made to determine the vortex breakdown characteristics of 43 str...
The YF-16 and F-16 developmental wind tunnel test program was reviewed. Geometrical descriptions, ge...
"July 1979"--Cover.Includes bibliographical references.v. 1. Summary and analysis / C.W. Smith, J.N....
Wind tunnel investigations have been conducted of forebody strakes for yaw control on 0.06-scale mod...
A propulsive wind/canard model was tested at STOL operating conditions in the NASA Langley Research ...
A propulsive wing/canard model was tested at STOL operating conditions in the NASA Langley Research ...
A low-speed wind tunnel investigation was conducted in the Langley 12-Foot Tunnel on a typical comme...
A general research fighter model was tested in the Langley 7 by 10 foot high speed tunnel at a Mach ...
Data were obtained with and without the nose boom and with several strake configurations; also, data...
The sixth scale model of the Sikorsky/NASA/Army rotor systems research aircraft was tested in an 18-...
Wind tunnel stability test of low aspect ratio delta winged model equipped with sharp-edged strake
Computations of drag polars for a low-speed Wortmann sailplane airfoil are compared to both wind tun...
A systematic wind tunnel study was conducted in the Langley high-speed 7 by 10 foot tunnel to docume...
The method described in this report is intended to present an overview of a process developed to ext...
For a body of revolution with afterbody side strakes, an experimental investigation was conducted in...
A systematic water-tunnel study was made to determine the vortex breakdown characteristics of 43 str...
The YF-16 and F-16 developmental wind tunnel test program was reviewed. Geometrical descriptions, ge...
"July 1979"--Cover.Includes bibliographical references.v. 1. Summary and analysis / C.W. Smith, J.N....
Wind tunnel investigations have been conducted of forebody strakes for yaw control on 0.06-scale mod...
A propulsive wind/canard model was tested at STOL operating conditions in the NASA Langley Research ...
A propulsive wing/canard model was tested at STOL operating conditions in the NASA Langley Research ...
A low-speed wind tunnel investigation was conducted in the Langley 12-Foot Tunnel on a typical comme...
A general research fighter model was tested in the Langley 7 by 10 foot high speed tunnel at a Mach ...
Data were obtained with and without the nose boom and with several strake configurations; also, data...
The sixth scale model of the Sikorsky/NASA/Army rotor systems research aircraft was tested in an 18-...
Wind tunnel stability test of low aspect ratio delta winged model equipped with sharp-edged strake
Computations of drag polars for a low-speed Wortmann sailplane airfoil are compared to both wind tun...
A systematic wind tunnel study was conducted in the Langley high-speed 7 by 10 foot tunnel to docume...
The method described in this report is intended to present an overview of a process developed to ext...
For a body of revolution with afterbody side strakes, an experimental investigation was conducted in...
A systematic water-tunnel study was made to determine the vortex breakdown characteristics of 43 str...