Explore Books on
supersonic nozzles

Turbulent-flow separation criteria for overexpanded supersonic nozzles

By E. Leon Morrisette

Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle

By Stephen W. D. Wolf

Introduction to molecular beams gas dynamics

By Giovanni Sanna,Giuseppe Tomassetti

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

By Steven P. Schneider

The flip-flop nozzle extended to supersonic flows

By Ganesh Raman

Exhaust nozzles for propulsion systems with emphasis on supersonic cruise aircraft

By Leonard E. Stitt

Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis

By Gregory Wayne Burgreen

Internal reversing flow in a tailpipe offtake configuration for SSTOVL aircraft

By Jack G. McArdle

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

By Richard S. Larson

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

By George T. Carson

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

By W. I. Scallion

An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code

By Mary Ann Dembowski

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

By Michael K. Ponton

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

By Laurence D. Leavitt

Optical techniques for determination of normal shock position in supersonic flows for aerospace applications

By Grigory Adamovsky

"Supersonic Gas-Liquid Cleaning System" research project

By Frank Kinney

Computation of supersonic jet noise under imperfectly expanded conditions

By Chan M. Kim

An atomic hydrogen supersonic nozzle beam source

By John Potjewyd

Analytical and experimental studies of sound suppressor components for NASA rocket engine test stands

By Washington State University. College of Engineering. Research Division.

The transonic flow in the throat region of a two-dimensional nozzle with walls of arbitrary smooth profile

By Alan William Moore

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

By L. H. Back

Design of a supersonic nozzle

By A. McCabe

Analysis of ejectors used as supersonic propelling nozzles for jet engines

By Bengt Ahrén

Raschet ėkstremalʹnoĭ formy sverkhzvukovoĭ chasti prostranstvennogo sopla

By Borisov, V. M.