共 50 条
- [3] CONSTANT-TEMPERATURE MAGNETO-GASDYNAMIC CHANNEL FLOW [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (01): : 78 - 78
- [4] The structure of gasdynamic flow in a supersonic separator of natural gas [J]. High Temperature, 2008, 46 : 69 - 76
- [6] SOME EXPLICIT SOLUTIONS FOR CONSTANT-TEMPERATURE MAGNETO-GASDYNAMIC CHANNEL FLOW [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1962, 29 (06): : 748 - 750
- [7] STATIONARY MAGNETO-GASDYNAMIC SHOCK IN HIGHLY UNDEREXPANDED CURRENT-CARRYING PLASMA JET [J]. ZEITSCHRIFT FUR ANGEWANDTE PHYSIK, 1971, 31 (01): : 65 - &
- [8] SIMILAR SOLUTIONS FOR BOUNDARY LAYERS IN CONSTANT-TEMPERATURE MAGNETO-GASDYNAMIC CHANNEL FLOW [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (02): : 156 - 157
- [9] Gasdynamic structure of a supersonic flow around a heat source [J]. ICIASF'01: 19TH INTERNATIONAL CONGRESS ON INSTRUMENTATION IN AEROSPACE SIMULATION FACILITIES, RECORD, 2001, : 70 - 81
- [10] The Flow Structure at Interaction of Gas Jets with Cross-Flow in the Supersonic Combustor [J]. INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2018), 2018, 2027