共 50 条
- [11] LOAD DISTRIBUTIONS ON DELTA-WINGS AT SUPERSONIC SPEEDS - REPLYJOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (11): : 792 - 792KAINER, JH
- [12] LEESIDE FLOWS OVER DELTA-WINGS AT SUPERSONIC SPEEDSJOURNAL OF AIRCRAFT, 1984, 21 (09): : 680 - 686MILLER, DSWOOD, RM
- [13] NONUNIFORM MOTION OF LEADING-EDGE VORTEX BREAKDOWN ON RAMP PITCHING DELTA-WINGSAIAA JOURNAL, 1992, 30 (07) : 1691 - 1702MIAU, JJCHANG, RCCHOU, JHLIN, CK
- [14] ESTIMATION OF ATTAINABLE LEADING-EDGE THRUST FOR WINGS AT SUBSONIC AND SUPERSONIC SPEEDS.NASA Technical Paper, 1979, (1500):Carlson, Harry W.Mack, Robert J.Barger, Raymond L.
- [15] HIGH-PERFORMANCE WINGS WITH SIGNIFICANT LEADING-EDGE THRUST AT SUPERSONIC SPEEDSJOURNAL OF AIRCRAFT, 1980, 17 (06): : 419 - 422ROBINS, AWCARLSON, HW
- [16] CONNECTION BETWEEN LEADING-EDGE SWEEP, VORTEX LIFT, AND VORTEX STRENGTH FOR DELTA-WINGSJOURNAL OF AIRCRAFT, 1990, 27 (05): : 473 - 475HEMSCH, MJLUCKRING, JM
- [17] SOME ROLL CHARACTERISTICS OF CRUCIFORM DELTA-WINGS AT SUPERSONIC SPEEDSJOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (05): : 289 - 297BLEVISS, ZO
- [18] IMPROVED CALCULATIONS OF LEADING-EDGE SEPARATION FROM SLENDER THIN DELTA WINGSPROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1968, 306 (1484): : 67 - &SMITH, JHB
- [19] Open-type separation on delta wings for leading-edge bluntnessTRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2007, 50 (168) : 81 - 87Chiba, KazuhisaObayash, ShigeruNakahashi, Kazuhiro
- [20] COMPUTATIONAL STUDY OF INCIPIENT LEADING-EDGE SEPARATION ON A SUPERSONIC DELTA WINGJOURNAL OF AIRCRAFT, 1992, 29 (02): : 203 - 209MCMILLIN, SNPITTMAN, JLTHOMAS, JL