共 50 条
- [1] THE FLOW OVER A WEDGE PROFILE AT MACH NUMBER-1JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (11): : 723 - 735GUDERLEY, GYOSHIHARA, H
- [2] OSCILLATING AIRFOILS AT MACH NUMBER-1JOURNAL OF THE AERONAUTICAL SCIENCES, 1949, 16 (06): : 380 - 381ROTT, N
- [3] 2-DIMENSIONAL UNSYMMETRIC FLOW PATTERNS AT MACH NUMBER-1JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (11): : 757 - 768GUDERLEY, GYOSHIHARA, H
- [4] ON SUPERSONIC FLOW PAST A FINITE WEDGE AT THE CROCCO MACH NUMBERJOURNAL OF THE AERONAUTICAL SCIENCES, 1955, 22 (04): : 261 - &TAMADA, KSHIBAOKA, Y
- [5] FLOW PAST A BENT PLATE WITH AN UNSYMMETRIC DEAD AIR AT MACH NUMBER-1JOURNAL OF THE PHYSICAL SOCIETY OF JAPAN, 1958, 13 (09) : 1055 - 1060SAKURAI, T
- [6] THE FLOW OVER A FLAT PLATE WITH A SMALL ANGLE OF ATTACK AT MACH NUMBER-1JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (04): : 261 - 274GUDERLEY, G
- [7] MAGNETOHYDRODYNAMIC WAVE OF FINITE AMPLITUDE AT MAGNETIC PRANDTL NUMBER-1PHYSICS OF FLUIDS, 1959, 2 (05) : 575 - 576HASIMOTO, H
- [8] RELIABILITY IS NUMBER-1I&CS-INDUSTRIAL AND PROCESS CONTROL MAGAZINE, 1983, 56 (11): : 25 - 25HICKEY, J
- [10] LIFT AND DRAG MEASUREMENTS ON A RECTANGULAR WING WITH SPLITTER WEDGE IN MACH NUMBER RANGE OF 0.5 TO 1.2ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1974, 22 (12): : 416 - 426TANNER, M