1-24 of 95 Books
Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle
Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle
By Stephen W. D. Wolf
User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel
User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel
By Ronald H. Soeder
NASA Lewis 8- by 6-foot supersonic wind tunnel user manual
NASA Lewis 8- by 6-foot supersonic wind tunnel user manual
By Ronald H. Soeder
Aeronautical facilities catalogue
Aeronautical facilities catalogue
By Frank E. Peñaranda
Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers
Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers
By George L. Stefko
Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research
Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research
By Steven P. Schneider
Wind-tunnel investigation of the validity of a sonic-boom-minimization concept
Wind-tunnel investigation of the validity of a sonic-boom-minimization concept
By Robert J. Mack
Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3
Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3
By Robert L. Stallings
Supersonic quiet-tunnel development for laminar-turbulent transition research
Supersonic quiet-tunnel development for laminar-turbulent transition research
By Steven P. Schneider
Correlation of predicted and measured sonic boom characteristics from the reentry of STS-1 Orbiter
Correlation of predicted and measured sonic boom characteristics from the reentry of STS-1 Orbiter
By Frank Garcia
Supersonic laminar flow control research
Supersonic laminar flow control research
By Ching F. Lo
Comparison of 3-D viscous flow computations of Mach 5 inlet with experimental data
Comparison of 3-D viscous flow computations of Mach 5 inlet with experimental data
By D. R. Reddy
Computational support of the lamimar [i.e. laminar] supersonic wind tunnel, CNSFV code development, Maglev, and grid generation
Computational support of the lamimar [i.e. laminar] supersonic wind tunnel, CNSFV code development, Maglev, and grid generation
By Goetz H. Klopfer
Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles
Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles
By Ivan E. Beckwith
An experimental device for generating high frequency perturbations in supersonic wind tunnels
An experimental device for generating high frequency perturbations in supersonic wind tunnels
By Kevin J. Melcher
NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6
NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6
By Stephen W. D. Wolf
Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds
Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds
By A. B. Blair
Flow quality and operational enhancements in the NASA Lewis 8- by 6-Foot Supersonic Wind Tunnel
Flow quality and operational enhancements in the NASA Lewis 8- by 6-Foot Supersonic Wind Tunnel
By E. Allen Arrington
Noise reduction in a Mach 5 wind tunnel with a rectangular rod-wall sound shield
Noise reduction in a Mach 5 wind tunnel with a rectangular rod-wall sound shield
By Theodore R. Creel
Analysis of the performance of the drive system and diffuser of the Langley Unitary Plan Wind Tunnel
Analysis of the performance of the drive system and diffuser of the Langley Unitary Plan Wind Tunnel
By Lowell E. Hasel
Wind-tunnel investigation of the validity of a sonic-boom-minimization concept
Wind-tunnel investigation of the validity of a sonic-boom-minimization concept
By Robert J Mack
Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel
Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel
By Theodore R. Creel
Subcommittee hearings on H. R. 3434, to promote the national defense by authorizing a unitary plan for the construction of transonic and supersonic wind-tunnel facilities and the establishment of an air engineering development center
Subcommittee hearings on H. R. 3434, to promote the national defense by authorizing a unitary plan for the construction of transonic and supersonic wind-tunnel facilities and the establishment of an air engineering development center
By United States. Congress. House. Committee on Armed Services. Subcommittee No. 3.