Magnetohydrodynamic Control of Hypersonic Flows and Scramjet Inlets Using Electron Beam Ionization
- 1 January 2002
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 40 (1), 74-81
- https://doi.org/10.2514/2.1616
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Electron-Beam-Generated Plasmas in Hypersonic Magnetohydrodynamic ChannelsAIAA Journal, 2001
- Potential performance of supersonic MHD power generatorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2001
- Supersonic air-scoop flows of a weakly ionized gas in external electromagnetic fieldTechnical Physics, 2000
- Comments on MHD energy bypass engine powered spacelinerPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- MHD power extraction from cold hypersonic air flow with external ionizersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- Electron beam generated plasmas in hypersonic MHD channelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- Electrode sheaths and boundary layers in hypersonic MHD channelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- Use of MHD systems in hypersonic aircraftTechnical Physics, 1998
- MHD acceleration of supersonic air flows using electron beam-enhanced conductivityPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Feasibility study of a hybrid MHD/radiatively driven facility for hypersonic ground testingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997