Computational Study of Near-Limit Propagation of Detonation in Hydrogen-Air Mixtures.
類似資料:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
テクニカルペーパー
Computational and Experimental Study of NOx Formation in Hydrogen-Fueled Pulse Detonation Engines
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
10
テクニカルペーパー
Numerical Study of Shock-Wave/Boundary Layer Interactions in Premixed Hydrogen-Air Hypersonic Flows
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
6
テクニカルペーパー
Thermodynamic Cycle and CFD Analyses for Hydrogen Fueled Air-Breathing Pulse Detonation Engines.
American Institute of Aeronautics and Astronautics |
12
テクニカルペーパー
Computation of dynamic parameters of detonation in hydrogen-air and propane-air mixtures using detailed chemistry
American Institute of Aeronautics and Astronautics |