Wind Tunnels

1,469 books
Dynamic measurement of total temperature, pressure, and velocity in the Langley 0.3-meter transomic cryogenic tunnelCharles B. Johnson

Dynamic measurement of total temperature, pressure, and velocity in the Langley 0.3-meter transomic cryogenic tunnel

Charles B. Johnson

1986No page data
Study of optical techniques for the Ames unitary wind tunnelsLee, George.

Study of optical techniques for the Ames unitary wind tunnels

Lee, George.

1992No page data
NASA Glenn 1-by 1-foot supersonic wind tunnel user manualUnknown Author

NASA Glenn 1-by 1-foot supersonic wind tunnel user manual

Unknown Author

1999No page data
A wall interference assessment/correction systemC. F. Lo

A wall interference assessment/correction system

C. F. Lo

1991No page data
Hot-jet simulation in cryogenic wind tunnelsKeisuke Asai
⏱ 45m

Hot-jet simulation in cryogenic wind tunnels

Keisuke Asai

198945 pp.
The F/A-18 high-angle-of-attack ground-to-flight correlationUnknown Author

The F/A-18 high-angle-of-attack ground-to-flight correlation

Unknown Author

1997No page data
Recommended PracticeAmerican Institute of Aeronautics and As
⏱ 1h 14m

Recommended Practice

American Institute of Aeronautics and As

200274 pp.
Langley 8-ft. HTT test 139 gas analysesDanny R. Sprinkle
⏱ 3h 12m

Langley 8-ft. HTT test 139 gas analyses

Danny R. Sprinkle

1999192 pp.
Slotted-wall flow-field measurements in a transonic wind tunnelJoel L. Everhart
⏱ 1h 45m

Slotted-wall flow-field measurements in a transonic wind tunnel

Joel L. Everhart

1991105 pp.
The NASA Langley 8-foot transonic pressure tunnel calibrationCuyler W. Brooks
⏱ 1h 9m

The NASA Langley 8-foot transonic pressure tunnel calibration

Cuyler W. Brooks

199469 pp.
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 wingThomas A. Byrdsong
⏱ 3h 31m

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

Thomas A. Byrdsong

1983211 pp.
NASA Lewis 8- by 6-foot supersonic wind tunnel user manualRonald H. Soeder

NASA Lewis 8- by 6-foot supersonic wind tunnel user manual

Ronald H. Soeder

1993No page data
KC-135 Winglet Program ReviewKC-135 Winglet Program Review (1981 Edwards, Calif.)

KC-135 Winglet Program Review

KC-135 Winglet Program Review (1981 Edwards, Calif.)

1982No page data
Semi-span model testing in the National Transonic FacilityNdaona Chokani

Semi-span model testing in the National Transonic Facility

Ndaona Chokani

1993No page data
The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnelPaul T. Soderman

The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel

Paul T. Soderman

1992No page data
NASA Lewis 9-by 15-foot low-speed wind tunnel user manualRonald H. Soeder

NASA Lewis 9-by 15-foot low-speed wind tunnel user manual

Ronald H. Soeder

1993No page data
Wind-tunnel techniqueR. C. Pankhurst
⏱ 11h 42m

Wind-tunnel technique

R. C. Pankhurst

1952702 pp.
The 13-inch magnetic suspension and balance system wind tunnelWilliam G. Johnson
⏱ 45m

The 13-inch magnetic suspension and balance system wind tunnel

William G. Johnson

198945 pp.
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8j to 90jUnknown Author

Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8j to 90j

Unknown Author

1983No page data
Wind-tunnel/flight correlation, 1981Unknown Author
⏱ 3h 52m

Wind-tunnel/flight correlation, 1981

Unknown Author

1982232 pp.
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