Explore Books on
wind tunnel models
1-24 of 81 Books
A wall interference assessment/correction system
A wall interference assessment/correction system
By C. F. Lo
Recommended Practice
By American Institute of Aeronautics and As
Semi-span model testing in the National Transonic Facility
Semi-span model testing in the National Transonic Facility
By Ndaona Chokani
Remote sensing of hydrologic variables in boreal areas
Remote sensing of hydrologic variables in boreal areas
By Eugene L. Peck
High-precision buffer circuit for suppression of regenerative oscillation
High-precision buffer circuit for suppression of regenerative oscillation
By John S. Tripp
Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode
Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode
By Michael B. Lance
Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
By Wendy B. Lessard
Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel
Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel
By P. S. Barna
Wind-tunnel investigation of an advanced general aviation canard configuration
Wind-tunnel investigation of an advanced general aviation canard configuration
By Joseph R. Chambers
Hot-bench simulation of the active flexible wing wind-tunnel model
Hot-bench simulation of the active flexible wing wind-tunnel model
By Carey S. Buttrill
Support interference of wind tunnel models
Support interference of wind tunnel models
By Marie H. Tuttle
A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process
A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process
By Daniel M. Vairo
A laser-based ice shape profilometer for use in icing wind tunnels
A laser-based ice shape profilometer for use in icing wind tunnels
By Edward A. Hovenac
Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique
Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique
By Daryl J. Monson
Stereo electro-optical tracking system (SETS)
Stereo electro-optical tracking system (SETS)
By Edward W. Koenig
A common geometric data-base approach for computer-aided manufacturing of wind-tunnel models and theoretical aerodynamic analysis
A common geometric data-base approach for computer-aided manufacturing of wind-tunnel models and theoretical aerodynamic analysis
By Michael J. See
Machining-induced deformation in stepped specimens of PH 13-8 Mo, 18 nickel maraging steel grade 200TI and grain-refined HP 9-4-20
Machining-induced deformation in stepped specimens of PH 13-8 Mo, 18 nickel maraging steel grade 200TI and grain-refined HP 9-4-20
By D. A. Wigley
The roll control of magnetically suspended wind tunnel models by transverse magnets
The roll control of magnetically suspended wind tunnel models by transverse magnets
By M. J. Goodyer
Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1)
Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1)
By Henry H Arnaiz
A common geometric data-base approach for computer-aided manufacturing of wind-tunnel models and theoretical aerodynamic analysis
A common geometric data-base approach for computer-aided manufacturing of wind-tunnel models and theoretical aerodynamic analysis
By Michael J See
Experimental aerothermodynamic research of hypersonic aircraft
Experimental aerothermodynamic research of hypersonic aircraft
By Joseph W. Cleary
Cryogenic wind tunnels
Cryogenic wind tunnels
By Marie H. Tuttle
Stereo electro-optical tracking system (SETS)
Stereo electro-optical tracking system (SETS)
By Edward W Koenig
Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
By William G. Johnson