Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers /

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

Full-scale thrust reverser testing in an altitude facility /
by: Mehalic, Charles M.
Published: (1987)

Internal thrust and pumping performance of an auxiliary inlet ejector nozzle with clamshell thrust reverser /
by: Mansour, Ali H., et al.
Published: (1969)

A performance comparison of two small rocket nozzles /
by: Arrington, Lynn A., et al.
Published: (1996)

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

Calibration for thrust and airflow measurements in the CE-22 Advanced Nozzle Test Facility /
by: Werner, Roger A.
Published: (2010)

Pressure measurements of impinging jet with asymmetric nozzle : progress report /
by: He, Zhiming
Published: (1988)

Pressure measurements of impinging jet with asymmetric nozzle : progress report /
by: He, Zhiming
Published: (1988)

Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles /
by: Mason, Mary L., et al.
Published: (1985)

Vacuum chamber pressure effects on thrust measurements of low Reynolds number nozzles /
Published: (1985)

Preliminary experiments on the noise generated by target-type thrust reverser models /
by: Gutierrez, Orlando A., et al.
Published: (1972)

Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility /
by: Wong, Kin C.
Published: (2003)

Converging-diverging nozzle thruster code for nuclear or chemical rocket performance computations /
by: Juhasz, Albert J.
Published: (2019)

Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure /
by: Hussaini, M. Moin, et al.
Published: (1996)

Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability /
by: Mason, Mary L., et al.
Published: (1986)

Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring" : June 11, 1989-December 10, 1989 /
by: Tseng, Jing-Biau
Published: (1989)

Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 /
by: Carson, George T., et al.
Published: (1988)

Separate flow nozzle test status meeting : proceedings of a conference held at and sponsored by NASA Glenn Research Center, Cleveland, Ohio, September 9-10, 1997 /
Published: (2000)

Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air /
by: Scallion, W. I.
Published: (1991)

Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊ /
by: Leavitt, Laurence D.
Published: (1985)

Decomposing solid micropropulsion nozzle performance issues /
by: Reed, Brian D.
Published: (2003)

Increased jet noise due to a "nominally laminar" state of nozzle exit boundary layer /
by: Zaman, K. B. M. Q. (Khairul B. M. Q.)
Published: (2017)

Static jet noise test results of four 0.35 scale-model QCGAT mixer nozzles /
by: Groesbeck, Donald E., et al.
Published: (1984)

Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles /
by: Yetter, Jeffery A., et al.
Published: (1980)

Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control /
by: Asbury, Scott C., et al.
Published: (1999)

'Trapped wave' resonances in jets from plug nozzles /
by: Fagan, Amy F., et al.
Published: (2024)

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., et al.
Published: (2000)

Multi-axis thrust measurements of the EO-1 pulsed plasma thruster /
by: Arrington, Lynn A., et al.
Published: (1999)

Noise from aft deck exhaust nozzles : differences in experimental embodiments /
by: Bridges, James E.
Published: (2014)

Near-exit pressure fluctuations in jets from circular and rectangular nozzles /
by: Zaman, K. B. M. Q. (Khairul B. M. Q.), et al.
Published: (2019)

Acoustic investigation of jet mixing noise in dual stream nozzles /
by: Khavaran, Abbas, 1953-, et al.
Published: (2012)

Flow processes in overexpanded chemical rocket nozzles.
by: Schmucker, Robert H.
Published: (1984)

A convergent nozzle for the standardisation of thrust-rig measurements /
by: Herbert, M. V.
Published: (1969)

A survey of challenges in aerodynamic exhaust nozzle technology for aerospace propulsion applications /
by: Shyne, Rickey J.
Published: (2002)

A survey of challenges in aerodynamic exhaust nozzle technology for aerospace propulsion applications /
by: Shyne, Rickey J.
Published: (2002)

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)