Nozzle Geometry

31 books
Two-dimensional converging-diverging rippled nozzles at transonic speedsJohn R. Carlson
⏱ 1h 45m

Two-dimensional converging-diverging rippled nozzles at transonic speeds

John R. Carlson

1994105 pp.
Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressureRobert S. Jankovsky

Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure

Robert S. Jankovsky

1996No page data
Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent airW. I. Scallion

Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air

W. I. Scallion

1991No page data
Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanesRobert J. Foley
⏱ 1h 17m

Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes

Robert J. Foley

199177 pp.
CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion systemIng Chuang

CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system

Ing Chuang

1997No page data
An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition ductBruce A. Reichert

An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct

Bruce A. Reichert

1991No page data
Analysis and design of optimized truncated scarfed nozzles subject to external flow effectsRickey J. Shyne
⏱ 10m

Analysis and design of optimized truncated scarfed nozzles subject to external flow effects

Rickey J. Shyne

199010 pp.
Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20George T. Carson
⏱ 2h 51m

Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20

George T. Carson

1988171 pp.
A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research CenterKenneth J. Davidian
⏱ 28m

A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center

Kenneth J. Davidian

198728 pp.
Decomposing solid micropropulsion nozzle performance issuesBrian D. Reed

Decomposing solid micropropulsion nozzle performance issues

Brian D. Reed

2003No page data
Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzleDavid W. Lam

Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle

David W. Lam

1995No page data
Investigation of ramp injectors for supersonic mixing enhancementY. Haimovitch

Investigation of ramp injectors for supersonic mixing enhancement

Y. Haimovitch

1994No page data
Space shuttle ice suppression system validationJ. L. F. Porteiro

Space shuttle ice suppression system validation

J. L. F. Porteiro

1983No page data
Computing axisymmetric jet screech tones using unstructured gridsPhilip C. E. Jorgenson

Computing axisymmetric jet screech tones using unstructured grids

Philip C. E. Jorgenson

2002No page data
Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flowsScott T. Imlay
⏱ 3h 0m

Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows

Scott T. Imlay

1986180 pp.
Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle conceptDavid J. Wing

Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept

David J. Wing

1994No page data
Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction controlScott C. Asbury

Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control

Scott C. Asbury

1999No page data
Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facilityKin C. Wong

Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility

Kin C. Wong

2003No page data
Ultra-high bypass ratio jet noiseLow, John, K. C.

Ultra-high bypass ratio jet noise

Low, John, K. C.

1994No page data
Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation caseJoseph F. Baumeister

Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case

Joseph F. Baumeister

1994No page data
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