Comparison of turbulence models for nozzle-afterbody flows with propulsive jets View on Open Library

Comparison of turbulence models for nozzle-afterbody flows with propulsive jets

by William B. Compton

No reviews yet
First published: 1996 1 language
Subjects
Aerodynamic coefficients Angle of attack Axisymmetric flow Computational fluid dynamics Convergent-divergent nozzles Exhaust gases Free flow Jet exhaust K-epsilon turbulence model Navier-Stokes equation

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by William B. Compton

Transonic Navier-Stokes solutions of three-dimensional afterbody flows

Transonic Navier-Stokes solutions of thr...

On the solution of the three-dimensional flowfield about a flow-through nacelle

On the solution of the three-dimensional...

You Might Also Like

More in Aerodynamic coeffici...
An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients

An initial investigation into methods of...

Leland A. Carlson
High-lift systems on commercial subsonic airliners

High-lift systems on commercial subsonic...

Peter K. C. Rudolph
2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall

2-D and 3-D oscillating wing aerodynamic...

R. A. Piziali
Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept

Evaluation of the low-speed stability an...

David E. Hahne
Hypersonic pitching-moment shift for stardust reentry capsule forebody

Hypersonic pitching-moment shift for sta...

William A. Wood
Two-dimensional high-lift aerodynamic optimization using neural networks

Two-dimensional high-lift aerodynamic op...

Roxana M. Greenman