Three dimensional flow computations and thrust predictions in 2DCD overexpanded nozzles-Reference-Cited by-同舟云学术

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Three dimensional flow computations and thrust predictions in 2DCD overexpanded nozzles

Published:1997-01-06 Issue: Volume: Page:
ISSN:
Container-title:35th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Hamed A.¹,Vogiatzis C.¹,Hamed A.¹,Vogiatzis C.¹

Affiliation:

1. Cincinnati, Univ., OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-30

Reference13 articles.

1. Capone,F.J."The NonaxisymmetricNozzle-Itis forReal",AIAA79-1810,August 1979.

2. Berrier, B.L., Palcza, J.L., Richey, G.K. "Nonaxisymmetric Nozzle Technology Program - AnOverview",AIAA77-1225,August 1977.

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2. Assessment of turbulence modeling for gas flow in two-dimensional convergent–divergent rocket nozzle;Applied Mathematical Modelling;2011-07

3. Assessment of multiscale resolution for hybrid turbulence model in unsteady separated transonic flows;Computers & Fluids;2007-06

4. 3-D Navier-Stokes simulation of turbulent afterbody/nozzle flows;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12

5. A parametric study of slot injection thrust vectoring in a 2DCD nozzle;33rd Joint Propulsion Conference and Exhibit;1997-07-06

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