Acoustic performance of an advanced model turbofan in three aeroacoustic test facilities /

Hybrid wing body shielding studies using an ultrasonic configurable fan artificial noise source generating typical turbofan modes /
by: Sutliff, Daniel L. (Daniel Linden), 1962-, et al.
Published: (2014)

The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator /
by: Hughes, Christopher E.
Published: (2013)

Performance optimization of a rotor alone Nacelle for acoustic fan testing /
by: Cunningham, C. C, et al.
Published: (2000)

Acoustic performance of drive rig mufflers for model scale engine testing /
by: Stephens, David B.
Published: (2013)

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)

Flow quality survey of the 8-by 6-foot supersonic wind tunnel (2015 test) prior to the 9-by 15-foot low-speed wind tunnel acoustic improvement modifications /
by: Johnson, Aaron M.
Published: (2018)

Acoustic directivity and insertion loss measurements of advanced liners installed in the inlet of the DGEN aeropropulsion research turbofan /
by: Sutliff, Daniel L., et al.
Published: (2019)

Core/combustor-noise measurements and source separation for the DGEN aeropropulsion research turbofan /
by: Hultgren, Lennart S. (Lennart Sven), et al.
Published: (2024)

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)

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

Takeoff/approach noise for a model counterrotation propeller with a forward-swept upstream rotor /
Published: (1993)

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 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)

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

A basic robotic excavator (the "Glenn digger٣) : description, design, and initial operation /
by: Bauman, Steve
Published: (2016)

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

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

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

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

An assessment of 3-C PIV analysis methodology for HART II measured data /
by: Lim, Joon W.
Published: (2010)

NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6 /
by: Wolf, Stephen W. D., et al.
Published: (1997)

Development of experimental icing simulation capability for full-scale swept wings : hybrid design process, years 1 and 2 /
by: Fujiwara, Gustavo
Published: (2017)

Rotating rake turbofan duct mode measurement system /
by: Sutliff, Daniel L. (Daniel Linden), 1962-
Published: (2005)

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

Wind turbine acoustics research : bibliography with selected annotation /
by: Hubbard, Harvey H., et al.
Published: (1988)

Two-dimensional wind tunnel.
Published: (1982)

Determination of HART I blade structural properties by laboratory testing /
by: Jung, Sung N., et al.
Published: (2012)

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

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

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

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

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

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

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

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

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