共 50 条
- [1] THE INCOMPRESSIBLE LAMINAR BOUNDARY LAYER ON A SPINNING CYLINDER AT SMALL ANGLES OF ATTACK PHYSICAL REVIEW, 1954, 96 (03): : 847 - 847
- [2] Heat Transfer in the Hypersonic Laminar Boundary Layer on a Cone with Zero Angle of Attack 4TH INTERNATIONAL CONFERENCE ON MATERIALS ENGINEERING FOR ADVANCED TECHNOLOGIES (ICMEAT 2015), 2015, : 212 - 214
- [3] LAMINAR BOUNDARY LAYER ON A SPINNING CONE AT SMALL ANGLES OF ATTACK IN A SUPERSONIC FLOW JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (06): : 430 - &
- [5] THE COMPRESSIBLE LAMINAR BOUNDARY LAYER JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (06): : 418 - 419
- [6] SEPARATION OF A LAMINAR BOUNDARY LAYER COMPTES RENDUS HEBDOMADAIRES DES SEANCES DE L ACADEMIE DES SCIENCES SERIE A, 1969, 268 (04): : 239 - &
- [8] ON A SOLUTION TO THE UNSTEADY LAMINAR BOUNDARY LAYER JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (06): : 474 - 474
- [9] TRANSITION IN A SEPARATED LAMINAR BOUNDARY LAYER JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (02): : 92 - 96
- [10] COMPUTATION OF THE LAMINAR BOUNDARY LAYER WITH SUCTION JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (01): : 48 - 54