Add to ORKGThe YF-16 and F-16 developmental wind tunnel test program was reviewed. Geometrical descriptions, general comments, representative data, and the initial efforts toward the development of design guides for the application of strakes to future aircraft are presented
An analytical strake design procedure is investigated. A numerical solution to the governing strake ...
A brief overview of a cooperative NASA/Boeing research effort, Strake Technology Research Applicatio...
The results from research on forebody vortex control on both the F/A-18 and the F-16 aircraft will b...
The YF-16 and F-16 developmental wind tunnel test program was reviewed and all force data pertinent ...
"July 1979"--Cover.Includes bibliographical references.v. 1. Summary and analysis / C.W. Smith, J.N....
A series of low-speed static wind-tunnel force tests were conducted on a 0.15-scale model of a moder...
Wind tunnel investigations have been conducted of forebody strakes for yaw control on 0.06-scale mod...
Low-speed wind-tunnel tests were conducted in the Langley 12-Foot Low-Speed Tunnel on a model of the...
A general research fighter model was tested in the Langley 7 by 10 foot high speed tunnel at a Mach ...
A systematic water-tunnel study was made to determine the vortex breakdown characteristics of 43 str...
A low-speed wind tunnel investigation was conducted in the Langley 12-Foot Tunnel on a typical comme...
A water-tunnel test of a 4.4 percent-scale, forebody-only model of the X-31 aircraft with different ...
A supersonic wind tunnel investigation was conducted in the NASA Langley Unitary Plan Wind Tunnel on...
The ability of current methodologies to accurately predict the aerodynamic characteristics identifie...
A systematic wind tunnel study was conducted in the Langley high-speed 7 by 10 foot tunnel to docume...
An analytical strake design procedure is investigated. A numerical solution to the governing strake ...
A brief overview of a cooperative NASA/Boeing research effort, Strake Technology Research Applicatio...
The results from research on forebody vortex control on both the F/A-18 and the F-16 aircraft will b...
The YF-16 and F-16 developmental wind tunnel test program was reviewed and all force data pertinent ...
"July 1979"--Cover.Includes bibliographical references.v. 1. Summary and analysis / C.W. Smith, J.N....
A series of low-speed static wind-tunnel force tests were conducted on a 0.15-scale model of a moder...
Wind tunnel investigations have been conducted of forebody strakes for yaw control on 0.06-scale mod...
Low-speed wind-tunnel tests were conducted in the Langley 12-Foot Low-Speed Tunnel on a model of the...
A general research fighter model was tested in the Langley 7 by 10 foot high speed tunnel at a Mach ...
A systematic water-tunnel study was made to determine the vortex breakdown characteristics of 43 str...
A low-speed wind tunnel investigation was conducted in the Langley 12-Foot Tunnel on a typical comme...
A water-tunnel test of a 4.4 percent-scale, forebody-only model of the X-31 aircraft with different ...
A supersonic wind tunnel investigation was conducted in the NASA Langley Unitary Plan Wind Tunnel on...
The ability of current methodologies to accurately predict the aerodynamic characteristics identifie...
A systematic wind tunnel study was conducted in the Langley high-speed 7 by 10 foot tunnel to docume...
An analytical strake design procedure is investigated. A numerical solution to the governing strake ...
A brief overview of a cooperative NASA/Boeing research effort, Strake Technology Research Applicatio...
The results from research on forebody vortex control on both the F/A-18 and the F-16 aircraft will b...