Sub-Alfvenic Inlet Boundary Conditions for Axisymmetric MHD Nozzles

Sub-Alfvenic Inlet Boundary Conditions for Axisymmetric MHD Nozzles

著者名:

J. Cassibry ( Propulsion Research Center, University of Alabama-Huntsville, Huntsville, AL )
S. Wu ( Center for Space Plasma and Aeronomy Research, University of Alabama-Huntsville, Huntsville, AL )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA Plasmadynamics and Lasers Conference

シリーズ巻号:

2006

発行年:

2006

通号:

2006-3561

ペーパー番号:

AIAA Paper 2006-3561

出版情報:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200612 [CD-ROM 2006 Disc 12]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047236
シリーズID:	PA00000148
会議名:	AIAA Plasmadynamics and Lasers Conference
回次:	37th
会議開催地:	San Francisco, California
会議開催年:	2006.06.05-2006.06.08

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1 テクニカルペーパー Theoretical Performance of an MHD Nozzle Using Super-Alfvenic Detachment J. Cassibry American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Validation of Inlet and Exhaust Boundary Conditions for a Cartesian Method Pandya, S., Murman, S., Aftosmis, M. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Comparison of Directly and Inductively Coupled Pulsed Electromagnetic Thrusters Cassibry, J., Wu, S. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー CFD Results for an Axisymmetric Isentropic Relaxed Compression Inlet S. Hirt, K. Tacina, T. Conners, J. Merret, D. Howe American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Effects of Propellant Injection, Material and Electrode Geometry on the Performance of a Two-Stage Pulsed Plasma Accelerator Cassibry, J., Markusic, T., Wu, S. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Integrated Simulations for Multi-Component Analysis of Gas Turbines:RANS Boundary Conditions Kim, S., Alonso, J., Schluter, J., Wu, X., Pitsch, H. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Effects of Equation of State and Transport on the Modeling of Pulsed Plasma Accelerators Cassibry, J., Markusic, T., Wu, S. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Improvement of disk MHD generator performance by inlet swirl Yamasaki, H., Okuno, Y., Torii, S., Masuda, J., Tsutsumi, M., Oda, N., Uchiyama, K., Kouka, H., Fujimoto, T., Suzuki, … American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Flow and Acoustics of a Coaxial Nozzle: a Sensitivity Study to the Inlet Boundary Conditions M. Mihaescu, E. Gutmark, R. Szasz, L. Fuchs American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Improvement of Disk MHD Generator Performance by Inlet Swirl Yamasaki, H., Okuno, Y., Torii, S., Masuda, J., Tsutsumi, M., Oda, N., Uchiyama, K., Kouka, H., Fujimoto, T., Suzuki, … American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Numerical Modeling Studies of Plasma Driven Magnetoinertial Fusion J. Cassibry, C. Knapp, R. Kirkpatrick, S. Wu American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Plume Diagnostics Supporting Magnetic Nozzle Plasma Detachment Demonstration Experiment B. Schuettpelz, Z. Li, J. Cassibry American Institute of Aeronautics and Astronautics

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