Nozzle Design

65 books
Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilitiesLaurence D. Leavitt
⏱ 1h 46m

Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities

Laurence D. Leavitt

1985106 pp.
Nozzle design optimization by method-of-characteristicsM. Going
⏱ 11m

Nozzle design optimization by method-of-characteristics

M. Going

199011 pp.
First NASA/Industry High Speed Research Program Nozzle SymposiumNASA/Industry High Speed Research Program Nozzle Symposium (1st 1992 Cleveland, Ohio)

First NASA/Industry High Speed Research Program Nozzle Symposium

NASA/Industry High Speed Research Program Nozzle Symposium (1st 1992 Cleveland, Ohio)

1999No page data
Contoured nozzle design and evaluation for hotshot wind tunnelsE. E. Edenfield
⏱ 13m

Contoured nozzle design and evaluation for hotshot wind tunnels

E. E. Edenfield

196813 pp.
A performance comparison of two small rocket nozzlesLynn A. Arrington

A performance comparison of two small rocket nozzles

Lynn A. Arrington

1996No page data
Perfect bell nozzle parametric and optimization curvesJ. L. Tuttle
⏱ 26m

Perfect bell nozzle parametric and optimization curves

J. L. Tuttle

198326 pp.
Design of an axisymmetric, contoured nozzle for the HEGKlaus Hannemann
⏱ 1h 11m

Design of an axisymmetric, contoured nozzle for the HEG

Klaus Hannemann

199071 pp.
An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzlesCraig A. Hunter

An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles

Craig A. Hunter

1995No page data
Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnelP. S. Barna

Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel

P. S. Barna

1995No page data
Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnelUnknown Author

Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnel

Unknown Author

1990No page data
Flight motor set 360L001 (STS-26R)Russell J. George

Flight motor set 360L001 (STS-26R)

Russell J. George

1989No page data
Design and evaluation of single and dual flow thrust vector nozzles with post exit vanesThomas W. Carpenter

Design and evaluation of single and dual flow thrust vector nozzles with post exit vanes

Thomas W. Carpenter

1992No page data
Design and evaluation of single and dual flow thrust vector nozzles with post exit vanesCarpenter, Thomas.

Design and evaluation of single and dual flow thrust vector nozzles with post exit vanes

Carpenter, Thomas.

1992No page data
Enhancement of mixing in a rectangular jet by mechanical tabsW. H. Brown

Enhancement of mixing in a rectangular jet by mechanical tabs

W. H. Brown

1990No page data
Space shuttle ice suppression system validationJ. L. F. Porteiro

Space shuttle ice suppression system validation

J. L. F. Porteiro

1984No page data
An aid to the design of orifice plates according to ISO code 5167T.R Fietz
⏱ 33m

An aid to the design of orifice plates according to ISO code 5167

T.R Fietz

198833 pp.
Shape optimization governed by the Euler equations using an adjoint methodAngelo Iollo
⏱ 18m

Shape optimization governed by the Euler equations using an adjoint method

Angelo Iollo

199318 pp.
The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flowsDarshan Dosanjh

The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows

Darshan Dosanjh

1995No page data
Raschet poteri t͡iagi prostranstvennykh sverkhzvukovykh sopel iz-za treni͡iaI. E. Mikhaĭlov
⏱ 25m

Raschet poteri t͡iagi prostranstvennykh sverkhzvukovykh sopel iz-za treni͡ia

I. E. Mikhaĭlov

199725 pp.
Design and checkout of a high speed research nozzle evaluation rigRaymond S. Castner

Design and checkout of a high speed research nozzle evaluation rig

Raymond S. Castner

1997No page data
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