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

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

By Robert J. Foley

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

By Scott C. Asbury

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

TMI-2 nozzle examinations performed at the Idaho National Laboratory

By D. W. Akers

Two-dimensional nozzle plume characteristics

By U. Von Glahn

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

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

By Nicholas Georgiadis

Wake adapted ducted propellers

By Marinus Willem Cornelis Oosterveld

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

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

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

By Scott T Imlay

Shape optimization governed by the Euler equations using an adjoint method

By Angelo Iollo

Design and Navier-Stokes analysis of hypersonic wind tunnel nozzles

By James R. Benton

Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20

By Francis J. Capone

Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps

By Laurence D. Leavitt

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

By Mary L. Mason

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

By William P. Henderson

Additional support for the TDK/MABL computer program

By Gary R. Nickerson