Measuring global surface pressures on a circulation control concept using pressure sensitive paint /

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

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)

Investigation of unsteady pressure-sensitive paint (uPSP) and a dynamic loads balance to predict launch vehicle buffet environments /
by: Schuster, D. M. (David M.)
Published: (2016)

Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel /
Published: (2011)

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)

Use of pressure sensitive paint for diagnostics in turbomachinery flows with shocks /
by: Lepicovsky, Jan
Published: (2001)

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)

Results from a pressure sensitive paint test conducted at the National Transonic Facility on test 197 : the common research model /
Published: (2011)

Using pressure sensitive paint to measure aerodynamic forces on a rotor blade in hover /
by: Watkins, Anthony Neal
Published: (2018)

Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow /
by: Hallissy, James B.
Published: (1989)

Pressure probe designs for dynamic pressure measurements in a supersonic flow field /
by: Porro, A. Robert
Published: (2001)

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

Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions /
by: Bartels, Robert E., et al.
Published: (1997)

Unified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields /
by: Erickson, Gary E.
Published: (2010)

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

Sidewall Mach number distributions for the NASA Langley Transonic Dynamics Tunnel /
by: Florance, James R.
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)

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)

Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil /
by: Watts, Michael E., et al.
Published: (1988)

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)

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

Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip /
by: Yeager, William T.
Published: (1997)

Pressure distribution for the wing of the YAV-8B airplane : with and without pylons /
by: Saltzman, Edwin J.
Published: (1992)

Rotor CFD analysis at terrestrial and martian atmospheric densities /
by: Perez Perez, Brenda Natalia
Published: (2018)

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

Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing /
by: Powers, Sheryll Goecke, et al.
Published: (1997)

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

An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients : semiannual progress report, January 1991 - June 1991 /
by: Carlson, Leland A.
Published: (1991)

Assessment of JVX proprotor performance data in hover and airplane-mode flight conditions /
by: Acree, C. W.
Published: (2016)

Experimental verification of buffet calculation procedure using unsteady PSP /
by: Panda, J. (Jayanta)
Published: (2016)

An experimental study of the turbulent boundary layer on a transport wing in subsonic and transonic flow /
by: Spaid, Frank W.
Published: (1990)

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