Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4 /

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)

Hot-bench simulation of the active flexible wing wind-tunnel model /
by: Buttrill, Carey S.
Published: (1990)

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

Design and calibration of the X-33 flush airdata sensing (FADS) system /
by: Whitmore, Stephen A., et al.
Published: (1998)

Modifications to the 4 x 7 meter tunnel for acoustic research : engineering feasibility study.
Published: (1986)

Measurements of fluctuating pressures in 8- by 6-foot supersonic wind tunnel for Mach number range of 0.56 to 2.07 /
by: Karabinus, Raymond J., et al.
Published: (1970)

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

Aeroservoelastic testing of free flying wind tunnel models /
by: Scott, Robert C.
Published: (2013)

Quantitative global heat transfer in a Mach-6 quiet tunnel /
by: Sullivan, John P.
Published: (2012)

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

Acoustic measurements from a rotor blade-vortex interaction noise experiment in the German-Dutch wind tunnel (DNW) /
by: Martin, R. M. (Ruth McVoy), 1956-
Published: (1988)

Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8 /
by: Davis, Mark C.
Published: (2000)

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)

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

Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack /
by: Cobleigh, Brent R., et al.
Published: (2001)

Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack /
by: Cobleigh, Brent R.
Published: (2001)

An aeroelastician's perspective of wind tunnel and flight experiences with active control of structural response and stability /
by: Hanson, Perry W.
Published: (1984)

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

14- by 22-foot subsonic tunnel laser velocimeter upgrade /
by: Meyers, James F.
Published: (2012)

The beginner's guide to wind tunnels with TunnelSim and TunnelSys /
by: Benson, Thomas J.
Published: (2010)

A wind-tunnel investigation at subsonic and low supersonic speeds of a re-entry vehicle with retractable wings /
by: Smith, Willard G.
Published: (1961)

Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform /
Published: (1990)

Estimation of aircraft nonlinear unsteady parameters from wind tunnel data /
by: Klein, Vladislav, et al.
Published: (1998)

Development of microchannel plates in advanced wind-tunnel instrumentation /
by: Feller, W. Bruce
Published: (1990)

Wind tunnel simulations of aeolian processes /
by: Greeley, Ronald
Published: (1984)

Digital-flutter-suppression-system investigations for the active flexible wing wind-tunnel model /
Published: (1990)

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

Tabulation of data from tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel /
by: Jenkins, Renaldo V.
Published: (1983)

Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /
by: Schuster, D. M. (David M.)
Published: (2001)

Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /
by: Schuster, D. M. (David M.)
Published: (2001)

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

The mothball, sustainment, and proposed reactivation of the hypersonic tunnel facility (HTF) at NASA Glenn Research Center Plum Brook Station /
by: Thomas, Scott R.
Published: (2010)

A wind tunnel study on the Mars Pathfinder (MPF) lander descent pressure sensor /
by: Soriano, J. Francisco
Published: (2001)

Subsonic and transonic pressure measurements on a high-aspect-ratio supercritical-wing model with oscillating control surfaces /
by: Sandford, M. C. (Maynard C.)
Published: (1981)

Dynamic response of a hammerhead launch vehicle wind-tunnel model /
by: Cole, Stanley R.
Published: (1991)

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