Unsteady-State Rocket Nozzle Flows-Reference-Cited by-同舟云学术

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Unsteady-State Rocket Nozzle Flows

Published:2002-07-07 Issue: Volume: Page:
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Container-title:38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Chang I-Shih

Publisher

American Institute of Aeronautics and Astronautics

Reference13 articles.

1. The Method of Space-Time Conservation Element and Solution Element—A New Approach for Solving the Navier-Stokes and Euler Equations

2. The Space-Time Conservation Element and Solution Element Method: A New High-Resolution and Genuinely Multidimensional Paradigm for Solving Conservation Laws

3. Chang, S. C., S. T. Yu, A. Himansu, X. Y. Wang, C. Y. Chow,andC.Y.Loh,"TheMethodofSpace-TimeConservationElementandSolutionElement-ANewParadigmforNumericalSolutionofConservationLaws,"ComputationalFluid Dynamics Review 1998, Vol.1, pp.206-240, World Scientific, Singapore, publ.

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. The a(3) Scheme---A Fourth-Order Neutrally Stable CESE Solver;18th AIAA Computational Fluid Dynamics Conference;2007-06-15

2. 3D Unsteady Navier-Stokes Rocket Nozzle Flows;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

3. Unsteady Navier-Stokes Rocket Nozzle Flows;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10

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