A basic robotic excavator (the "Glenn digger٣) : description, design, and initial operation /

Acoustic performance of an advanced model turbofan in three aeroacoustic test facilities /
by: Woodward, Richard P.
Published: (2012)

Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities /
by: Leavitt, Laurence D.
Published: (1985)

Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability /
by: Bangert, Linda S.
Published: (1989)

Flow-visualization techniques used at high speed by configuration aerodynamics wind-tunnel-test team /
Published: (2001)

Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept /
by: Riley, Donald R.
Published: (1989)

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)

Static performance of six innovative thrust reverser concepts for subsonic transport applications : summary of the NASA Langley Innovative Thrust Reverser Test Program /
by: Asbury, Scott C.
Published: (2000)

Icing cloud calibration of the NASA Glenn Icing Research Tunnel /
by: Ide, Robert F., et al.
Published: (2001)

Icing cloud calibration of the NASA Glenn Icing Research Tunnel /
by: Ide, Robert F.
Published: (2001)

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

An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner /
by: Arbiter, Dorothy G.
Published: (1985)

Acoustic testing of a high-tip-speed fan with bypass-duct liners--overview /
by: Miller, C. J. (Christopher J.), et al.
Published: (2019)

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

Hover test vehicle : implementation plan and test results.
Published: (2009)

Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° /
by: Berrier, Bobby L., et al.
Published: (1984)

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)

Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan /
by: Hughes, Christopher E.
Published: (2013)

Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF /
by: Perkins, H. Douglas, et al.
Published: (1996)

Analysis of small-scale rotor hover performance data /
by: Kitaplioglu, Cahit
Published: (1990)

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)

Initial investigation of the acoustics of a counter-rotating open rotor model with historical baseline blades in a low-speed wind tunnel /
by: Elliott, David M.
Published: (2012)

Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode /
by: Lance, Michael B.
Published: (1991)

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

Experimental sonic boom measurements on a Mach 1.6 cruise low-boom configuration /
by: Wilcox, Floyd J.
Published: (2012)

Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight /
by: Thomas, Scott R., et al.
Published: (1997)

Performance test results of the NASA-457M v2 Hall thruster /
by: Soulas, George C. (George Chris), 1966-
Published: (2012)

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

Results of design studies and wind tunnel tests of an advanced high lift system for an energy efficient transport /
by: Oliver, Wayne R.
Published: (1980)

Low-speed stability-and-control and ground-effects measurements on the industry reference high speed civil transport /
by: Kennerly, Guy T.
Published: (1999)

Model engine performance measurement from force balance instrumentation /
by: Jeracki, Robert J.
Published: (1998)

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

Cruise noise of the SR-2 propeller model in a wind tunnel /
by: Dittmar, James H.
Published: (1989)

A wind tunnel study of icing effects on a business jet airfoil /
Published: (2003)

Cruise noise of the SR-2 propeller model in a wind tunnel /
by: Dittmar, James H.
Published: (1989)

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

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)