共 50 条
- [41] VISCOUS INFLUENCE IN AXISYMMETRIC LAMINAR SUPERSONIC-FLOW OVER BLUNT BODIES [J]. ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1985, 65 (04): : T216 - T218
- [45] NONUNIFORM SUPERSONIC-FLOW PAST WEDGES [J]. ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND PHYSIK, 1973, 24 (03): : 355 - 364
- [46] A SCHEME FOR COMPUTING NEAR-AXISYMMETRICAL GAS-FLOW AND SUPERSONIC-FLOW PAST A CYLINDER END-FACE AT A LOW-ANGLE OF ATTACK [J]. USSR COMPUTATIONAL MATHEMATICS AND MATHEMATICAL PHYSICS, 1986, 26 (03): : 200 - 203
- [47] SUPERSONIC-FLOW ABOUT CIRCULAR CONES AT LARGE ANGLES OF ATTACK - FLOATING DISCONTINUITY APPROACH [J]. ASTRONAUTICS & AERONAUTICS, 1977, 15 (10): : B8 - B8
- [48] COMMENTS ON SUPERSONIC FLOW AT THE SURFACE OF A CIRCULAR CONE AT ANGLE OF ATTACK [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1962, 29 (04): : 481 - 482
- [49] THE OPTIMUM-OPTIMORUM SHAPE OF THE INTEGRATED WING-FUSELAGE CONFIGURATION IN SUPERSONIC-FLOW [J]. ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1988, 68 (05): : T324 - T327
- [50] CONICAL FLARINGS IN UNIFORM SUPERSONIC FLOW AT ZERO ANGLE OF ATTACK [J]. AIAA JOURNAL, 1963, 1 (04) : 950 - 950