Global Model of Liquid Rocket Engine Combustion Instability Based on Chemistry Dynamics.
類似資料:
American Institute of Aeronautics and Astronautics |
7
テクニカルペーパー
Flowrate and acoustics characteristics of coaxial swirling injector of hydrogen/oxygen rocket engine
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
テクニカルペーパー
Numerical simulation of unsteady flow in liquid propellant rocket engine with PISO algorithm
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 |
American Institute of Aeronautics and Astronautics |