Numerical simulation of flow separation in rocket nozzle-Reference-Cited by-同舟云学术

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Numerical simulation of flow separation in rocket nozzle

Published:1997-05 Issue:3 Volume:24 Page:269-276
ISSN:0093-6413
Container-title:Mechanics Research Communications
language:en
Short-container-title:Mechanics Research Communications

Author:

Hadjadj A.,Nebbache A.,Vuillamy D.,Vandromme D.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science,Civil and Structural Engineering

Reference10 articles.

1. Application and validation of the FL3D solver to propulsion flows;Bobba;AIAA paper 94–0656,1994

2. Computation of separated and unsteady flows with one and two equation turbulence models;Ekaterinaris;AIAA paper, 94–0190,1994

3. Thin layer approximation and algebraic model for separated turbulent flows;Baldwin;AIAA paper, 78–0257,1978

4. Navier-stokes solutions for an axisymmetric nozzle;Hasen;AIAA J,1982

5. Current status of numerical solution of the Navier-Stokes equations;Maccormack;AIAA paper 85-0032,1985

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical Characterisation of Supersonic Exhaust Diffusers;Defence Science Journal;2017-03-14

2. Radiative Heat Transfer in Film-Cooled Liquid Rocket Engine Nozzles;Journal of Thermophysics and Heat Transfer;2003-01

3. Study of radiative heat transfer in film cooled LH/LO rocket engines thrust chamber;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14

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