共 50 条
- [32] PREDICTION OF AXISYMMETRIC TURBULENT BOUNDARY-LAYER IN CONICAL NOZZLES JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1974, 41 (01): : 20 - 24
- [39] SHOCK BEAMING CAPABILITIES OF HYDRODYNAMIC CONICAL SHOCK TUBES JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1971, 50 (05): : 1313 - &
- [40] Shock patterns in the plume of overexpanded rocket nozzles PROCEEDINGS OF THE THIRD EUROPEAN SYMPOSIUM ON AEROTHERMODYNAMICS FOR SPACE VEHICLES, 1999, 420 : 395 - 402