Leading-edge separations and cross-flow shocks on delta wings
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[1] Michael J. Siclari,et al. Investigation of Crossflow Shocks on Delta Wings in Supersonic Flow , 1979 .
[2] H. Thomann. Measurement of heat transfer, recovery temperature, and pressure distribution on delta wings at M=3(1) , 1963 .
[3] L C Squire,et al. Flow Regimes over Delta Wings at Supersonic and Hypersonic Speeds , 1976 .
[4] A. Stanbrook,et al. Possible Types of Flow at Swept Leading Edges , 1964 .
[5] L. C. Squire,et al. The motion of a thin oil sheet under the steady boundary layer on a body , 1961, Journal of Fluid Mechanics.
[6] R. Korkegi. On the Structure of Three-Dimensional Shock-Induced Separated Flow Regions , 1976 .
[7] William H. Mason,et al. Controlled supercritical crossflow on supersonic wings - An experimental validation , 1980 .
[8] David J. Peake,et al. Three-dimensional interactions and vortical flows with emphasis on high speeds , 1980 .
[9] J. Szodruch. Reynolds number influence on leeside flowfields , 1978 .
[10] J. G. Szodruch. Leeward flow over delta wings at supersonic speeds , 1980 .
[11] L. C. Squire. The characteristics of some slender cambered gothic wings at Mach numbers from 0.4 to 2.0 , 1962 .
[12] J. N. Hefner,et al. Lee-surface vortex effects over configurations in hypersonic flow. , 1972 .