Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles /

Exhaust nozzle plume and shock wave interaction /
by: Castner, Raymond S., et al.
Published: (2013)

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

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

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

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

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

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

Analysis and design of optimized truncated scarfed nozzles subject to external flow effects /
by: Shyne, Rickey J.
Published: (1990)

Exhaust environment measurements of a turbofan engine equipped with an afterburner and 2D nozzle /
by: Brase, L. O.
Published: (1990)

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)

Experimental evaluation of a translating nozzle sidewall radial turbine /
by: Roelke, Richard J.
Published: (1987)

Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine /
by: Paxson, Daniel E.
Published: (2015)

Mach 5 electroformed nickel nozzle refurbishment : FNAS investigation of ultra-smooth surfaces /
by: Rood, Robert, et al.
Published: (1992)

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)

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

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

Methodology for three dimensional nozzle design /
by: Ferri, Aldo A., et al.
Published: (1974)

Exit boundary layer data for a round convergent nozzle in support of numerical simulation efforts /
by: Zaman, K. B. M. Q. (Khairul B. M. Q.)
Published: (2019)

Shelf life extension for the lot AAE nozzle severance LSCs : final test report /
by: Cook, M.
Published: (1990)

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)

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

Supersonic wind tunnel nozzles : a selected, annotated bibliography to aid in the development of quiet wind tunnel technology /
by: Wolf, Stephen W. D.
Published: (1990)

Computational simulations of convergent nozzles for the AIAA 1st Propulsion Aerodynamics Workshop /
by: Dippold, Vance
Published: (2014)

Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet /
by: Ponton, Michael K., et al.
Published: (1999)

Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers /
by: Green, Robert S.
Published: (1987)

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)

Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers /
by: Green, Robert S.
Published: (1987)

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)

An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct /
by: Reichert, Bruce A.
Published: (1991)

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

CFD analysis of nozzle jet plume effects on sonic boom signature /
by: Bui, Trong T.
Published: (2009)

Acoustic measurements of rectangular nozzles with bevel /
by: Bridges, James E., 1943-
Published: (2012)

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

Multidisciplinary approach to aerospike nozzle design /
by: Korte, J. J.
Published: (1997)