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transonic wind tunnels

1-24 of 132 Books

View Slotted-wall flow-field measurements in a transonic wind tunnel By Joel L. Everhart

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

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

By Joel L. Everhart

View The NASA Langley 8-foot transonic pressure tunnel calibration By Cuyler W. Brooks

The NASA Langley 8-foot transonic pressure tunnel calibration

The NASA Langley 8-foot transonic pressure tunnel calibration

By Cuyler W. Brooks

View Assessment of dual-point drag reduction for an executive-jet modified airfoil section By Dennis O. Allison

Assessment of dual-point drag reduction for an executive-jet modified airfoil section

Assessment of dual-point drag reduction for an executive-jet modified airfoil section

By Dennis O. Allison

View Control of the NASA Langley 16-foot transonic tunnel with the self-organizing feature map By Mark A. Motter

Control of the NASA Langley 16-foot transonic tunnel with the self-organizing feature map

Control of the NASA Langley 16-foot transonic tunnel with the self-organizing feature map

By Mark A. Motter

View High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions By Julio Chu

High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions

High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions

By Julio Chu

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

View Evaluation of flow quality in two large NASA wind tunnels at transonic speeds By Bill Harvey

Evaluation of flow quality in two large NASA wind tunnels at transonic speeds

Evaluation of flow quality in two large NASA wind tunnels at transonic speeds

By Bill Harvey

View Computation of imaginary-side pressure distributions over the flexible walls of the test section insert for the 0.3-M transonic cryogenic tunnel By M. J. Goodyer

Computation of imaginary-side pressure distributions over the flexible walls of the test section insert for the 0.3-M transonic cryogenic tunnel

Computation of imaginary-side pressure distributions over the flexible walls of the test section insert for the 0.3-M transonic cryogenic tunnel

By M. J. Goodyer

View Sidewall boundary-layer measurements with upstream suction in the Langley 0.3-meter transonic cryogenic tunnel By A. V. Murthy

Sidewall boundary-layer measurements with upstream suction in the Langley 0.3-meter transonic cryogenic tunnel

Sidewall boundary-layer measurements with upstream suction in the Langley 0.3-meter transonic cryogenic tunnel

By A. V. Murthy

View Simulation of ideal-gas flow by nitrogen and other selected gases at cyogenic temperatures By Robert M. Hall

Simulation of ideal-gas flow by nitrogen and other selected gases at cyogenic temperatures

Simulation of ideal-gas flow by nitrogen and other selected gases at cyogenic temperatures

By Robert M. Hall

View Combustibility tests of 1,1,1,2-tetrafluoroethane in a simulated compressor cylinder By Dale A. Babcock

Combustibility tests of 1,1,1,2-tetrafluoroethane in a simulated compressor cylinder

Combustibility tests of 1,1,1,2-tetrafluoroethane in a simulated compressor cylinder

By Dale A. Babcock

View A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel By Edward T. Schairer

A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel

A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel

By Edward T. Schairer

View Demonstration of imaging flow diagnostics using Rayleigh scattering in Langley 0.3-Meter Transonic Cryogenic Tunnel By B. Shirinzadeh

Demonstration of imaging flow diagnostics using Rayleigh scattering in Langley 0.3-Meter Transonic Cryogenic Tunnel

Demonstration of imaging flow diagnostics using Rayleigh scattering in Langley 0.3-Meter Transonic Cryogenic Tunnel

By B. Shirinzadeh

View Stereo electro-optical tracking system (SETS) By Edward W. Koenig

Stereo electro-optical tracking system (SETS)

Stereo electro-optical tracking system (SETS)

By Edward W. Koenig

View Performance of the 0.3-meter transonic cryogenic tunnel with air, nitrogen, and sulfer hexafluoride media under closed loop automatic control By Balakrishna, S.

Performance of the 0.3-meter transonic cryogenic tunnel with air, nitrogen, and sulfer hexafluoride media under closed loop automatic control

Performance of the 0.3-meter transonic cryogenic tunnel with air, nitrogen, and sulfer hexafluoride media under closed loop automatic control

By Balakrishna, S.

View The new heavy gas testing capability in the NASA Langley Transonic Dynamics Tunnel By Stanley R. Cole

The new heavy gas testing capability in the NASA Langley Transonic Dynamics Tunnel

The new heavy gas testing capability in the NASA Langley Transonic Dynamics Tunnel

By Stanley R. Cole

View 16-foot transonic tunnel test section flowfield survey By J. A. Yetter

16-foot transonic tunnel test section flowfield survey

16-foot transonic tunnel test section flowfield survey

By J. A. Yetter

View Transonic dynamics tunnel force and pressure data acquired on the HSR rigid semispan model By D. M. Schuster

Transonic dynamics tunnel force and pressure data acquired on the HSR rigid semispan model

Transonic dynamics tunnel force and pressure data acquired on the HSR rigid semispan model

By D. M. Schuster

View Boundary layer simulation and control in wind tunnels By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

Boundary layer simulation and control in wind tunnels

Boundary layer simulation and control in wind tunnels

By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

View The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel By M. C. Lewis

The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel

The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel

By M. C. Lewis

View Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel By Gregory V. Selby

Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel

Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel

By Gregory V. Selby

View Stereo electro-optical tracking system (SETS) By Edward W Koenig

Stereo electro-optical tracking system (SETS)

Stereo electro-optical tracking system (SETS)

By Edward W Koenig

View Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability By David J. Wing

Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability

Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability

By David J. Wing

View 16-foot transonic tunnel test section flowfield survey By Jeffery A. Yetter

16-foot transonic tunnel test section flowfield survey

16-foot transonic tunnel test section flowfield survey

By Jeffery A. Yetter