Comparison of computational codes for modeling hydrogen-oxygen injectors
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American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
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Finite splitter plate effects on flame holding in a confined hydrogen-oxygen shear layer
American Institute of Aeronautics and Astronautics |
9
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The Use of Asymptotic Expansions to Assess the Accuracy of Euler and Navier-Stokes Computations
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
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Computational Modeling of Instabilities in a Single-Element Rocket Combustor Using a Response Function
American Institute of Aeronautics and Astronautics |