共 50 条
- [1] Design-oriented leading-edge thrust force prediction for supersonic lifting surfaces JOURNAL OF AIRCRAFT, 1997, 34 (04): : 457 - 464
- [2] INFLUENCE OF LEADING-EDGE THRUST ON TWISTED AND CAMBERED WING DESIGN FOR SUPERSONIC CRUISE JOURNAL OF AIRCRAFT, 1983, 20 (05): : 440 - 445
- [4] ACOUSTIC INVESTIGATION OF LEADING-EDGE SERRATIONS ON LIFTING SURFACES JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1971, 50 (01): : 121 - &
- [5] ESTIMATION OF SUPERSONIC LEADING-EDGE THRUST BY A EULER FLOW MODEL JOURNAL OF AIRCRAFT, 1995, 32 (03): : 684 - 686
- [6] Computational Evaluation of the Performance of Lifting Surfaces with Leading-Edge Protuberances JOURNAL OF AIRCRAFT, 2011, 48 (02): : 591 - 600
- [7] WING DESIGN WITH ATTAINABLE LEADING-EDGE THRUST CONSIDERATIONS JOURNAL OF AIRCRAFT, 1985, 22 (03): : 244 - 248
- [8] ESTIMATION OF ATTAINABLE LEADING-EDGE THRUST FOR WINGS AT SUBSONIC AND SUPERSONIC SPEEDS. NASA Technical Paper, 1979, (1500):
- [9] HIGH-PERFORMANCE WINGS WITH SIGNIFICANT LEADING-EDGE THRUST AT SUPERSONIC SPEEDS JOURNAL OF AIRCRAFT, 1980, 17 (06): : 419 - 422
- [10] SIMPLIFIED VORTEX MODELS FOR SLENDER LIFTING SURFACES WITH LEADING-EDGE SEPARATION ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG, 1980, 4 (05): : 267 - 279