Explore Books on
wind tunnels
1-24 of 563 Books
Study of optical techniques for the Ames unitary wind tunnels
Study of optical techniques for the Ames unitary wind tunnels
By Lee, George.
Recommended Practice
By American Institute of Aeronautics and As
Hot-jet simulation in cryogenic wind tunnels
Hot-jet simulation in cryogenic wind tunnels
By Keisuke Asai
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
By Thomas A. Byrdsong
Wind Tunnel Testing of High-Rise Buildings
Wind Tunnel Testing of High-Rise Buildings
By Peter Irwin
Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊
Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊
By Emma Jean Landrum
KC-135 Winglet Program Review
KC-135 Winglet Program Review
By KC-135 Winglet Program Review (1981 Edwards, Calif.)
Langley 8-ft. HTT test 139 gas analyses
Langley 8-ft. HTT test 139 gas analyses
By Danny R. Sprinkle
Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊
Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊
By Emma Jean Landrum
Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results
Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results
By L. Tracy Redd
The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel
The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel
By Paul T. Soderman
Wind-tunnel test of an articulated helicopter rotor model with several tip shapes
Wind-tunnel test of an articulated helicopter rotor model with several tip shapes
By John D. Berry
The 13-inch magnetic suspension and balance system wind tunnel
The 13-inch magnetic suspension and balance system wind tunnel
By William G. Johnson
Wind-tunnel investigation of an advanced general aviation canard configuration
Wind-tunnel investigation of an advanced general aviation canard configuration
By Joseph R. Chambers
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
Aeronautical facilities catalogue
Aeronautical facilities catalogue
By Frank E. Peñaranda
Validation of vortex-lattice method for loads on wings in lift-generated wakes
Validation of vortex-lattice method for loads on wings in lift-generated wakes
By Vernon J. Rossow
A three-dimensional orthogonal laser velocimeter for the NASA Ames 7- by 10-foot wind tunnel
A three-dimensional orthogonal laser velocimeter for the NASA Ames 7- by 10-foot wind tunnel
By Stephen E. Dunagan
NASA Lewis 9-by 15-foot low-speed wind tunnel user manual
NASA Lewis 9-by 15-foot low-speed wind tunnel user manual
By Ronald H. Soeder
X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results
X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results
By Albion H. Bowers
Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers
Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers
By Timothy R. Moes
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
By Thomas A Byrdsong