Explore Books on
nozzles

Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles

By P. D. Thomas

Two-dimensional converging-diverging rippled nozzles at transonic speeds

By John R. Carlson

Turbofan forced mixer-nozzle internal flowfield

By Robert W. Paterson

High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation

By Robert S. Jankovsky

Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle

By Scott C. Asbury

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

By Robert J. Foley

Venturi nozzle effects on fuel drop size and nitrogen oxide emissions

By Susan M. Johnson

Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20

By Lawrence E. Putnam

Flight effects on the aerodynamic and acoustic characteristics of inverted profile coannular nozzles

By Hilary Kozlowski

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

By Scott T. Imlay

Use of Navier-Stokes methods for the calculation of high-speed nozzle flow fields

By Nicholas Georgiadis

Computation of three-dimensional nozzle-exhaust flow fields with the GIM code / L. W. Spradley, P. G. Anderson, and M. L. Pearson

By L. W. Spradley

Two-dimensional nozzle plume characteristics

By U. Von Glahn

TMI-2 nozzle examinations performed at the Idaho National Laboratory

By D. W. Akers

Wake adapted ducted propellers

By Marinus Willem Cornelis Oosterveld

Computation of three-dimensional nozzle-exhaust flow fields with the GIM code / L. W. Spradley, P. G. Anderson, and M. L. Pearson

By L. W Spradley

Hydraulic experiments with valves, orifices, hose, nozzles, and orifice buckets

By University of Illinois (Urbana-Champaign campus). Hydraulic Laboratory.

Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊

By Scott C. Asbury

Nuclear thermal rocket nozzle testing and evaluation program

By Kenneth O. Davidian

First NASA/Industry High Speed Research Program Nozzle Symposium

By First NASA/Industry High Speed Research Program Nozzle Symposium (1992 Cleveland, Ohio)

Experimental performance of three design factors for ventral nozzles for SSTOVL aircraft

By Barbara S. Esker

Experimental performance of a ventral nozzle with pitch and yaw vectoring capability for SSTOVL aircraft

By Barbara S. Esker

Low thrust viscous nozzle flow fields prediction

By G. S. Liaw

Analysis of film cooling in rocket nozzles

By Keith Woodbury