A CONCEPT OF THE VORTEX LIFT OF SHARP-EDGE DELTA WINGS BASED ON A LEADING-EDGE-SUCTION ANALOGY By
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[1] W. H. Wentz,et al. An experimental investigation of the flow fields about delta and double-delta wings at low speeds , 1966 .
[2] D. G. Koenig,et al. Experimental and theoretical studies of wing-leading-edge vortex flow , 1966 .
[3] B. Pershing. SEPARATED FLOW PAST SLENDER DELTA WINGS WITH SECONDARY VORTEX SIMULATION , 1964 .
[4] J. A. Lawford,et al. LOW-SPEED WIND-TUNNEL MEASUREMENTS ON A THIN SHARP-EDGED DELTA WING WITH 70 DEGREES LEADING-EDGE SWEEP, WITH PARTICULAR REFERENCE TO THE POSITION OF LEADING-EDGE VORTEX BREAKDOWN , 1961 .
[5] K. Gersten,et al. CALCULATION OF NON-LINEAR AERODYNAMIC STABILITY DERIVATIVES OF AEROPLANES , 1961 .
[6] Robert Thomas Jones,et al. High speed wing theory , 1960 .
[7] J. H. B. Smith,et al. A theory of the flow past a slender delta wing with leading edge separation , 1959, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.
[8] R. J. Vidal,et al. Experimental Investigation of Influence of Edge Shape on the Aerodynamic Characteristics of Low Aspect Ratio Wings at Low Speeds , 1955 .
[9] Clinton E. Brown,et al. On slender delta wings with leading-edge separation , 1955 .
[10] H. Multhopp. Methods for Calculating the Lift Distribution of Wings (Subsonic Lifting-Surface Theory). , 1950 .
[11] Louis P Tosti,et al. Low-speed static stability and damping-in-roll characteristics of some swept and unswept low-aspect-ratio wings , 1947 .
[12] William Bollay,et al. A Non-linear Wing Theory and its Application to Rectangular Wings of Small Aspect Ratio , 1939 .