Explore Books on
nozzles

Two-dimensional converging-diverging rippled nozzles at transonic speeds

By John R. Carlson

Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles

By P. D. Thomas

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

Two-dimensional nozzle plume characteristics

By U. Von Glahn

TMI-2 nozzle examinations performed at the Idaho National Laboratory

By D. W. Akers

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

Venturi nozzle effects on fuel drop size and nitrogen oxide emissions

By Susan M. Johnson

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

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

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

By Nicholas Georgiadis

Analysis of film cooling in rocket nozzles

By Keith Woodbury

Wake adapted ducted propellers

By Marinus Willem Cornelis Oosterveld

Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds

By William P. Henderson

A bibliographical survey of flow through orifices and parallel-throated nozzles

By Thomas Henry Redding

Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards

By Mary L. Mason

Development of a code for wall contour design in the transonic region of axisymmetric and square nozzles

By Timothy Alcenius

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

Additional support for the TDK/MABL computer program

By Gary R. Nickerson

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

By Barbara S. Esker

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

By Barbara S. Esker