1-24 of 132 Books
Slotted-wall flow-field measurements in a transonic wind tunnel
Slotted-wall flow-field measurements in a transonic wind tunnel
By Joel L. Everhart
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
The NASA Langley 8-foot transonic pressure tunnel calibration
The NASA Langley 8-foot transonic pressure tunnel calibration
By Cuyler W. Brooks
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
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
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
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
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
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
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
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
Stereo electro-optical tracking system (SETS)
Stereo electro-optical tracking system (SETS)
By Edward W. Koenig
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
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
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.
Subcommittee hearings on H. R. 3434, to promote the national defense by authorizing a unitary plan for the construction of transonic and supersonic wind-tunnel facilities and the establishment of an air engineering development center
Subcommittee hearings on H. R. 3434, to promote the national defense by authorizing a unitary plan for the construction of transonic and supersonic wind-tunnel facilities and the establishment of an air engineering development center
By United States. Congress. House. Committee on Armed Services. Subcommittee No. 3.
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
Full Committee Hearing on H.R. 9612 and S. 3889
Full Committee Hearing on H.R. 9612 and S. 3889
By United States. Congress. Senate. Committee on Armed Services.
Stereo electro-optical tracking system (SETS)
Stereo electro-optical tracking system (SETS)
By Edward W Koenig
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
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
16-foot transonic tunnel test section flowfield survey
16-foot transonic tunnel test section flowfield survey
By J. A. Yetter
Image degradation in Langley 0.3-meter transonic cryogenic tunnel
Image degradation in Langley 0.3-meter transonic cryogenic tunnel
By W. L. Snow