Wind Tunnel Nozzles

45 books
Design and Navier-Stokes analysis of hypersonic wind tunnel nozzlesJames R. Benton

Design and Navier-Stokes analysis of hypersonic wind tunnel nozzles

James R. Benton

1989No page data
Supersonic wind tunnel nozzlesStephen W. D. Wolf
⏱ 1h 19m

Supersonic wind tunnel nozzles

Stephen W. D. Wolf

199079 pp.
A summary of the techniques of variable Mach number supersonic wind tunnel nozzle designJ. T. Kenney
⏱ 2h 13m

A summary of the techniques of variable Mach number supersonic wind tunnel nozzle design

J. T. Kenney

1954133 pp.
A simple flexible supersonic wind tunnell nozzle for the rapid and accurate variation of flow mach numberD. Pierce
⏱ 10m

A simple flexible supersonic wind tunnell nozzle for the rapid and accurate variation of flow mach number

D. Pierce

196710 pp.
Method of characteristics design of a supersonic wind tunnel nozzle with square cross-sectionSteven P. Schneider

Method of characteristics design of a supersonic wind tunnel nozzle with square cross-section

Steven P. Schneider

1993No page data
Performance of a Mach 4 axially symmetric nozzle designed to operate at 40 microns hg. in the UTIA low density wind tunnelA. K. Sreekanth
⏱ 25m

Performance of a Mach 4 axially symmetric nozzle designed to operate at 40 microns hg. in the UTIA low density wind tunnel

A. K. Sreekanth

195625 pp.
Two-dimensional converging-diverging rippled nozzles at transonic speedsJohn R. Carlson
⏱ 1h 45m

Two-dimensional converging-diverging rippled nozzles at transonic speeds

John R. Carlson

1994105 pp.
Supersonic quiet-tunnel development for laminar-turbulent transition researchSteven P. Schneider

Supersonic quiet-tunnel development for laminar-turbulent transition research

Steven P. Schneider

1995No page data
Design of a new contraction for the ARL low speed wind tunnel (U)J. H. Watmuff
⏱ 21m

Design of a new contraction for the ARL low speed wind tunnel (U)

J. H. Watmuff

198621 pp.
Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF4 TunnelThompson, Richard A.
⏱ 29m

Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF4 Tunnel

Thompson, Richard A.

198729 pp.
Design of a high Reynolds number Mach number 8 contoured nozzle for the hypervelocity wind tunnel (F)Emmett E. Edenfield
⏱ 39m

Design of a high Reynolds number Mach number 8 contoured nozzle for the hypervelocity wind tunnel (F)

Emmett E. Edenfield

197239 pp.
Thermal/structural analysis of transpiration cooled nozzleUnknown Author

Thermal/structural analysis of transpiration cooled nozzle

Unknown Author

1992No page data
A preliminary investigation of the use of expanders to generate hypersonic flow in a wind tunnelH. Y. T. Wong
⏱ 14m

A preliminary investigation of the use of expanders to generate hypersonic flow in a wind tunnel

H. Y. T. Wong

196014 pp.
Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnelP. S. Barna

Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel

P. S. Barna

1995No page data
Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition researchSteven P. Schneider

Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research

Steven P. Schneider

1994No page data
Contoured nozzle design and evaluation for hotshot wind tunnelsE. E. Edenfield
⏱ 13m

Contoured nozzle design and evaluation for hotshot wind tunnels

E. E. Edenfield

196813 pp.
Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzleStephen W. D. Wolf

Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle

Stephen W. D. Wolf

1991No page data
Design of an axisymmetric, contoured nozzle for the HEGKlaus Hannemann
⏱ 1h 11m

Design of an axisymmetric, contoured nozzle for the HEG

Klaus Hannemann

199071 pp.
A de Laval nozzle for Mach number sevenNorman B. Tucker
⏱ 24m

A de Laval nozzle for Mach number seven

Norman B. Tucker

195224 pp.
Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflectorScott C. Asbury

Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector

Scott C. Asbury

1997No page data
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