Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /

An airfoil flutter model suspension system to accommodate large static transonic airloads /
by: Reed, Wilmer H.
Published: (1985)

A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel /
by: Lawing, Pierce L., et al.
Published: (1980)

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

Control of the NASA Langley 16-foot transonic tunnel with the self-organizing feature map /
by: Motter, Mark A.
Published: (1998)

Modeling and control study of the NASA 0.3-meter transonic cryogenic tunnel for use with sulfur hexafluoride medium /
by: Balakrishna, S.
Published: (1992)

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)

Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles /
by: Castner, Raymond S.
Published: (2010)

Aerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses /
by: Harris, Charles D., 1952-
Published: (1972)

Methodology of blade unsteady pressure measurement in the NASA transonic flutter cascade /
by: Lepicovsky, Jan
Published: (2002)

Methodology of blade unsteady pressure measurement in the NASA transonic flutter cascade /
Published: (2002)

Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel /
by: Johnson, William G. (William Garland), 1944-
Published: (1985)

Cryogenic pressure calibrator for wide temperature electronically scanned (ESP) pressure modules /
by: Faulcon, Nettie D.
Published: (2001)

Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment /
by: Harris, Charles D., 1952-, et al.
Published: (1988)

Flow quality surveys in the settling chamber of the NASA Glenn icing research tunnel (2011 tests) /
by: Steen, Laura E.
Published: (2014)

Pressure- and temperature-sensitive paint at 0.3-m transonic cryogenic tunnel /
by: Watkins, A. Neal
Published: (2015)

Design study of advanced model support systems for the National Transonic Facility.
Published: (1987)

A vapor generator for transonic flow visualization /
by: Bruce, Robert A.
Published: (1989)

A wall interference assessment/correction interface measurement system for the NASA-ARC 12-FT PWT : final memorandum report.
Published: (1989)

Two-dimensional wind tunnel.
Published: (1982)

Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations /
by: Hess, R. W. (Robert W.), et al.
Published: (1986)

Modifications to Langley 0.3-m TCT adaptive wall software for heavy gas test medium.
by: Murthy, A. V.
Published: (1992)

Finite element analysis of a NASA National Transonic Facility wind tunnel balance /
by: Lindell, Michael C.
Published: (1996)

Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel /
by: Hall, Robert M.
Published: (1979)

MAVRIC flutter model transonic limit cycle oscillation test /
Published: (2001)

MAVRIC flutter model transonic limit cycle oscillation test /
by: Edwards, John W.
Published: (2001)

Background pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel /
by: Castner, Raymond S.
Published: (2013)

Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel /
by: Selby, Gregory V. (Gregory Vincent)
Published: (1986)

An evaluation of three experimental processes for two-dimensional transonic tests /
by: Zuppardi, Gennaro
Published: (1989)

An evaluation of three experimental processes for two-dimensional transonic tests /
by: Zuppardi, Gennaro
Published: (1989)

Final report on investigation of transonic flow over segmented slotted wind tunnel wall with mass transfer /
by: Bhat, M. K.
Published: (1990)

A historical overview of Aeroelasticity Branch and Transonic Dynamics Tunnel contributions to rotorcraft technology and development /
by: Yeager, William T.
Published: (2001)

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

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

Three-dimensional flow field measurements in a transonic turbine cascade /
by: Giel, P. W.
Published: (1996)

Summary of the 2017 blockage test in the 10- by 10-foot supersonic wind tunnel /
by: Pastor-Barsi, Christine, 1982-, et al.
Published: (2018)

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