共 50 条
- [2] REMARKS ON CONICAL SUPERSONIC WINGS WITH SUBSONIC LEADING EDGES JOURNAL OF AIRCRAFT, 1978, 15 (05): : 319 - 320
- [3] LIFTING WINGS WITH MIXED (SUBSONIC-SUPERSONIC) LEADING EDGES AERONAUTICAL QUARTERLY, 1970, 21 (NOV): : 355 - &
- [5] LIFT DISTRIBUTION ON SUPERSONIC WINGS WITH SUBSONIC LEADING EDGES AND ARBITRARY ANGLE OF ATTACK DISTRIBUTION JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (11): : 783 - 785
- [6] NOTE ON THE EXTENSION OF EVVARD METHOD TO WINGS WITH SUBSONIC LEADING EDGES MOVING AT SUPERSONIC SPEEDS AERONAUTICAL QUARTERLY, 1957, 8 (01): : 87 - 102
- [7] AERODYNAMIC ANALYSIS OF SUPERSONIC AIRCRAFT WITH SUBSONIC LEADING EDGES JOURNAL OF AIRCRAFT, 1978, 15 (07): : 399 - 406
- [8] 3-DIMENSIONAL VISUALIZATIONS OF THE AERODYNAMIC CHARACTERISTICS OF DELTA WINGS FOR THE TRANSITION FROM SUBSONIC TO SUPERSONIC LEADING EDGES IN SUPERSONIC-HYPERSONIC FLOW ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1992, 72 (05): : T392 - T395
- [9] PROBLEM OF MINIMAL DRAG OF CONICAL SUPERSONIC WING SURFACES WITH SUBSONIC LEADING EDGES INGENIEUR ARCHIV, 1976, 45 (03): : 179 - 191
- [10] ON THE CONCEPTUAL DESIGN OF SUPERSONIC CRUISING AIRCRAFT WITH SUBSONIC WING LEADING EDGES. Delft progress report, 1983, 8 (01): : 55 - 80