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Explore Books on
subsonic wind tunnels

1-16 of 16 Books

View The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel By Norbert Ulbrich

The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel

The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel

By Norbert Ulbrich

View The 13-inch magnetic suspension and balance system wind tunnel By William G. Johnson

The 13-inch magnetic suspension and balance system wind tunnel

The 13-inch magnetic suspension and balance system wind tunnel

By William G. Johnson

View Subsonic aerodynamic assessment of vortex flow management devices on a high-speed civil transport configuration By Bryan A. Campbell

Subsonic aerodynamic assessment of vortex flow management devices on a high-speed civil transport configuration

Subsonic aerodynamic assessment of vortex flow management devices on a high-speed civil transport configuration

By Bryan A. Campbell

View Study of the unsteady flow features on a stalled wing By S. Yon

Study of the unsteady flow features on a stalled wing

Study of the unsteady flow features on a stalled wing

By S. Yon

View Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms By Kevin J. Kjerstad

Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms

Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms

By Kevin J. Kjerstad

View Effect of collector configuration on test section turbulence levels in an open-jet wind tunnel By Gregory S. Manuel

Effect of collector configuration on test section turbulence levels in an open-jet wind tunnel

Effect of collector configuration on test section turbulence levels in an open-jet wind tunnel

By Gregory S. Manuel

View Modification of the Ames 40- by 80-foot wind tunnel for component acoustic testing for the second generation supersonic transport By Fredric H. Schmitz

Modification of the Ames 40- by 80-foot wind tunnel for component acoustic testing for the second generation supersonic transport

Modification of the Ames 40- by 80-foot wind tunnel for component acoustic testing for the second generation supersonic transport

By Fredric H. Schmitz

View The Langley 14- by 22-foot subsonic tunnel: description, flow characteristics, and guide for users By Garl L. Gentry

The Langley 14- by 22-foot subsonic tunnel: description, flow characteristics, and guide for users

The Langley 14- by 22-foot subsonic tunnel: description, flow characteristics, and guide for users

By Garl L. Gentry

View A universal three-dimensional wall pressure correction method for closed rectangular subsonic wind tunnel test sections (displacement, downwash, streamline curvature) By Gerhard Schulz

A universal three-dimensional wall pressure correction method for closed rectangular subsonic wind tunnel test sections (displacement, downwash, streamline curvature)

A universal three-dimensional wall pressure correction method for closed rectangular subsonic wind tunnel test sections (displacement, downwash, streamline curvature)

By Gerhard Schulz

View Use of a scale model in the design of modifications to the NASA Glenn Icing Research Tunnel By Victor A. Canacci

Use of a scale model in the design of modifications to the NASA Glenn Icing Research Tunnel

Use of a scale model in the design of modifications to the NASA Glenn Icing Research Tunnel

By Victor A. Canacci

View Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel By Sharon S. Graves

Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel

Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel

By Sharon S. Graves

View Design of a new contraction for the ARL low speed wind tunnel (U) By J. H. Watmuff

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

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

By J. H. Watmuff

View Automatic control study of the icing research tunnel refrigeration system By Arthur E. Kieffer

Automatic control study of the icing research tunnel refrigeration system

Automatic control study of the icing research tunnel refrigeration system

By Arthur E. Kieffer

View Design & fabrication of a traversing mechanism and glide slope mechanism for the UTIAS wind tunnel By Hussein Amr Sabbour

Design & fabrication of a traversing mechanism and glide slope mechanism for the UTIAS wind tunnel

Design & fabrication of a traversing mechanism and glide slope mechanism for the UTIAS wind tunnel

By Hussein Amr Sabbour

View Subsonic wind-tunnel measurements of a slender wind-body configuration employing a vortex flap By Neal T. Frink

Subsonic wind-tunnel measurements of a slender wind-body configuration employing a vortex flap

Subsonic wind-tunnel measurements of a slender wind-body configuration employing a vortex flap

By Neal T. Frink

View The use of panel methods for the development of low subsonic wall interference and blockage corrections By K. G. Bowcutt

The use of panel methods for the development of low subsonic wall interference and blockage corrections

The use of panel methods for the development of low subsonic wall interference and blockage corrections

By K. G. Bowcutt