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- [2] COMMENTS ON SUPERSONIC FLOW AT THE SURFACE OF A CIRCULAR CONE AT ANGLE OF ATTACKJOURNAL OF THE AEROSPACE SCIENCES, 1962, 29 (04): : 481 - 482WOODS, BA
- [3] COMMENTS ON SUPERSONIC FLOW AT THE SURFACE OF A CIRCULAR CONE AT ANGLE OF ATTACK - REPLYJOURNAL OF THE AEROSPACE SCIENCES, 1962, 29 (04): : 482 - 482WILLETT, JE
- [4] Theoretical and Experimental Investigation of Supersonic Flow Past a Slender Sharp Circular Cone at IncidenceFLUID DYNAMICS, 2003, 38 (01) : 105 - 114Bashkin, V. A.Egorov, I. V.Ivanov, D. V.Plyashechnik, V. I.
- [5] Theoretical and Experimental Investigation of Supersonic Flow Past a Slender Sharp Circular Cone at IncidenceFluid Dynamics, 2003, 38 : 105 - 114V. A. BashkinI. V. EgorovD. V. IvanovV. I. Plyashechnik
- [6] LAMINAR BOUNDARY LAYER ON A CONE AT INCIDENCE IN SUPERSONIC FLOWAIAA JOURNAL, 1971, 9 (03) : 462 - &BOERICKE, RR
- [7] A NOTE ON THE INVISCID STREAMLINES AT THE SURFACE OF A YAWED CONE IN A SUPERSONIC STREAMJOURNAL OF THE AEROSPACE SCIENCES, 1962, 29 (03): : 375 - 376WILLETT, JE
- [8] THE SUPERSONIC-HYPERSONIC FLOW AROUND A CIRCULAR CONE WITH NORMAL BLOWING OR SUCTION THROUGH THE SURFACEMECHANICS RESEARCH COMMUNICATIONS, 1974, 1 (04) : 239 - 244Carafoli, E.Berbente, C.
- [9] SUPERSONIC-FLOW OF A VIBRATIONALLY RELAXING GAS PAST A CIRCULAR CONEJOURNAL OF FLUID MECHANICS, 1978, 85 (APR) : 519 - 542KAO, JHODGSON, JP
- [10] Initiation and development of separated flow behind a circular cylinder in a supersonic streamFluid Dynamics, 1998, 33 (6) : 833 - 841Bashkin V.A.Egorov I.V.Egorova M.V.Ivanov D.V.