An investigation of the causes of failure of flexible thermal protection materials in an aerodynamic environment /

Thermal/structural analysis of the shaft disk region of a fan drive system /
by: Gregory, Peyton B.
Published: (1990)

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

Mach 10 experimental database of a three-dimensional scramjet inlet flow field /
by: Holland, Scott D.
Published: (1995)

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

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

Shock generation and control using DBD plasma actuators : SBIR phase I final report /
by: Patel, Mehul P.
Published: (2012)

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

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

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

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)

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)

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

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)

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

Measuring global surface pressures on a circulation control concept using pressure sensitive paint /
Published: (2012)

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)

Measured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet /
by: Maglieri, Domenic J.
Published: (2011)

Exhaust nozzle plume effects on sonic boom test results for isolated nozzles /
by: Castner, Raymond S.
Published: (2011)

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

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

Experimental and computational sonic boom assessment of Boeing N+2 low boom models /
by: Durston, D. A.
Published: (2015)

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

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

Langley 16-ft. Transonic Tunnel Pressure Sensitive Paint System /
Published: (2001)

Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system /
by: DeBonis, J. R.
Published: (2001)

Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system /
by: DeBonis, James R., et al.
Published: (2001)

Thermal enclosures for electronically scanned pressure modules operating in cryogenic environments /
by: Mitchell, Michael
Published: (1989)

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

Comparison of analytical methods for calculation of wind loads /
by: Minderman, Donald J.
Published: (1989)

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)

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

Comprehensive report of fan performance from duct rake instrumentation on 1.294 pressure ratio, 806 ft/sec tip speed turbofan simulator models /
by: Jeracki, Robert J.
Published: (2006)

CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report /
by: Vinci, Samuel J.
Published: (2012)

Shock wave interaction with an abrupt area change /
by: Salas, M. D.
Published: (1991)

Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel /
by: Re, Richard J., et al.
Published: (1998)

Structural analysis of a thermal insulation retainer assembly /
by: Greene, William H.
Published: (1989)