Supersonic Nozzles

114 books
The flip-flop nozzle extended to supersonic flowsGanesh Raman

The flip-flop nozzle extended to supersonic flows

Ganesh Raman

1992No page data
Internal reversing flow in a tailpipe offtake configuration for SSTOVL aircraftJack G. McArdle

Internal reversing flow in a tailpipe offtake configuration for SSTOVL aircraft

Jack G. McArdle

1992No page data
Exhaust nozzles for propulsion systems with emphasis on supersonic cruise aircraftLeonard E. Stitt
⏱ 1h 43m

Exhaust nozzles for propulsion systems with emphasis on supersonic cruise aircraft

Leonard E. Stitt

1990103 pp.
Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speedsLaurence D. Leavitt
⏱ 2h 13m

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds

Laurence D. Leavitt

1979133 pp.
Turbulent-flow separation criteria for overexpanded supersonic nozzlesE. Leon Morrisette
⏱ 36m

Turbulent-flow separation criteria for overexpanded supersonic nozzles

E. Leon Morrisette

197836 pp.
Aerodynamic and acoustic investigation of inverted velocity profile coannular exhaust nozzle models and development of aerodynamic and acoustic prediction proceduresRichard S. Larson
⏱ 3h 36m

Aerodynamic and acoustic investigation of inverted velocity profile coannular exhaust nozzle models and development of aerodynamic and acoustic prediction procedures

Richard S. Larson

1979216 pp.
Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition researchSteven P. Schneider

Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research

Steven P. Schneider

1994No page data
Experimental and analytical investigation of axisymmetric supersonic cruise nozzle geometry at Mach numbers form 0.60 to 1.30George T. Carson
⏱ 1h 26m

Experimental and analytical investigation of axisymmetric supersonic cruise nozzle geometry at Mach numbers form 0.60 to 1.30

George T. Carson

198186 pp.
Far-field acoustics of supersonic rectangular nozzles with various aspect ratiosMichael K. Ponton

Far-field acoustics of supersonic rectangular nozzles with various aspect ratios

Michael K. Ponton

1987No page data
Methods of approximating inviscid jet boundaries for highly underexpanded supersonic nozzlesJ. R. Henson
⏱ 51m

Methods of approximating inviscid jet boundaries for highly underexpanded supersonic nozzles

J. R. Henson

196251 pp.
Comparisons of experimental with predicted wall static-pressure distributions in conical supersonic nozzlesL. H. Back
⏱ 17m

Comparisons of experimental with predicted wall static-pressure distributions in conical supersonic nozzles

L. H. Back

196417 pp.
Design of a supersonic nozzleA. McCabe
⏱ 37m

Design of a supersonic nozzle

A. McCabe

196737 pp.
The performance of a conical convergent-divergent nozzle with area ratio 2.9 in external flowG. T. Golesworthy
⏱ 12m

The performance of a conical convergent-divergent nozzle with area ratio 2.9 in external flow

G. T. Golesworthy

196712 pp.
The performance of conical convergent-divergent nozzles of area ratios 2.44 and 2.14 in external flowG. T. Golesworthy

The performance of conical convergent-divergent nozzles of area ratios 2.44 and 2.14 in external flow

G. T. Golesworthy

1967No page data
The effect of external flow on an internal-expansion propelling nozzle incorporating ventilation by ambient airHerbert, M. V.
⏱ 18m

The effect of external flow on an internal-expansion propelling nozzle incorporating ventilation by ambient air

Herbert, M. V.

196618 pp.
The performance of a centrebody propelling nozzle with a parallel shroud in external flowUnknown Author

The performance of a centrebody propelling nozzle with a parallel shroud in external flow

Unknown Author

1966No 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
Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speedsLaurence D. Leavitt
⏱ 2h 13m

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds

Laurence D. Leavitt

1979133 pp.
Effects of spanwise nozzle geometry and location on the longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speedsLaurence D. Leavitt
⏱ 1h 14m

Effects of spanwise nozzle geometry and location on the longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds

Laurence D. Leavitt

197874 pp.
Computation of supersonic jet noise under imperfectly expanded conditionsChan M. Kim

Computation of supersonic jet noise under imperfectly expanded conditions

Chan M. Kim

1993No page data
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