Design and calibration of the mixing layer and wind tunnel /

Investigation of materials for boundary layer control in a supersonic wind tunnel /
by: Braafladt, Alexander C., et al.
Published: (2013)

The NASA Langley 16-foot transonic tunnel : historical overview, facility description, calibration, flow characteristics, and test capabilities /
Published: (1995)

Performance tests for the NASA Ames Research Center 20 cm x 40 cm oscillating flow wind tunnel : progress report /
by: Cook, William John, 1929-
Published: (1984)

Flow unsteadiness effects on boundary layers /
by: Murthy, Sreedhara V.
Published: (1989)

Calibration of the NASA Glenn 8- by 6-foot supersonic wind tunnel (1996 and 1997 tests) /
by: Arrington, E. Allen
Published: (2012)

An experimental device for generating high frequency perturbations in supersonic wind tunnels /
by: Melcher, Kevin J., et al.
Published: (1996)

Study of the integration of wind tunnel and computational methods for aerodynamic configurations /
by: Browne, Lindsay E.
Published: (1989)

Experimental studies of transonic flow field near a longitudinally slotted wind tunnel wall /
by: Everhart, Joel L.
Published: (1994)

A planar reacting shear layer system for the study of fluid dynamics-combustion interaction /
Published: (1990)

Experimental study of boundary layer behavior in a simulated low pressure turbine /
by: Shyne, Rickey J.
Published: (1998)

Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels /
by: Ross, James C. (James Carl), 1955-
Published: (1989)

Experimental investigation of Mars Science Laboratory entry vehicle aeroheating in AEDC hypervelocity tunnel 9 /
by: Hollis, Brian R. (Brian Ray), et al.
Published: (2017)

Flow quality survey of the 8-by 6-foot supersonic wind tunnel (2015 test) prior to the 9-by 15-foot low-speed wind tunnel acoustic improvement modifications /
by: Johnson, Aaron M.
Published: (2018)

A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel /
by: Schairer, Edward T.
Published: (1989)

Simulation investigation of the effect of the NASA Ames 80- by 120-foot wind tunnel exhaust flow on light aircraft operating in the Moffett Field traffic pattern /
by: Streeter, Barry G.
Published: (1986)

Experimental parametric study of jet vortex generators for flow separation control /
by: Selby, Gregory V. (Gregory Vincent)
Published: (1991)

De-icing of the altitude wind tunnel turning vanes by electro-magnetic impulse /
by: Zumwalt, G. W.
Published: (1986)

NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6 /
by: Wolf, Stephen W. D., et al.
Published: (1997)

Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows /
Published: (1991)

Compressibility considerations for [kappa-omega] turbulence models in hypersonic boundary layer applications /
by: Rumsey, C. L. (Christopher Lockwood), 1961-
Published: (2009)

Contraction design for small low-speed wind tunnels /
by: Bell, J. H.
Published: (1988)

Contraction design for small low-speed wind tunnels /
by: Bell, J. H.
Published: (1988)

Development of a large field of view shadowgraph system for a 16 ft. transonic wind tunnel /
by: Talley, Michael A.
Published: (2000)

The effects of forcing on a single stream shear layer and its parent boundary layer /
by: Haw, Richard C.
Published: (1990)

The Langley 14- by 22-foot subsonic tunnel : description, flow characteristics, and guide for users /
Published: (1990)

Factors influencing pitot probe centerline displacement in a turbulent supersonic boundary layer /
by: Grosser, Wendy I.
Published: (1997)

Wind tunnel investigation of the supersonic stage separation aerodynamics of a generic 0.0175- scale bimese two-stage-to-orbit reusable launch vehicle configuration /
by: Erickson, Gary E.
Published: (2020)

Results of the AFRSI rewaterproofing systems screening test in the NASA/AMES Research Center (ARC) 2x2-foot transonic wind tunnel (OS-310) /
by: Marroquin, J., et al.
Published: (1985)

An experimental investigation on location of boundary layer transition on the NACA 0012 using surface hot film gages /
by: Wang, Tie-cheng
Published: (1986)

1-by 1- foot supersonic wind tunnel sidewall flowfield compression plate study /
by: Peters, Christopher J. (Christopher John), et al.
Published: (2020)

Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 /
by: Stallings, Robert L., et al.
Published: (1980)

Plume dispersion of the exhaust from a cryogenic wind tunnel /
by: Lassiter, William S.
Published: (1987)

Wind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena /
by: Kegerise, Michael A., et al.
Published: (2016)

Force instrumentation for cryogenic wind tunnels using one-piece strain-gage balances /
by: Ferris, Alice T.
Published: (1980)

Inviscid spatial stability of a compressible mixing layer.
by: Jackson, Thomas L. (Thomas Luther), 1957-
Published: (1989)

Inviscid spatial stability of a compressible mixing layer.
by: Jackson, Thomas L. (Thomas Luther), 1957-
Published: (1989)