Geodesic
Aerodynamic characteristics of $\Lambda$-shaped wings at subsonic speeds of flight
Vestnik Moskovskogo universiteta. Matematika, mehanika, no. 1 (1983), pp. 89-91

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The discrete eddies method is used for solving the problem of determining the airdynamic characteristics of a thin $\Lambda$-shaped wing for Mach number $M=0$ considering the flow stall from the leading edge. 
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     author = {V. I. Voronin},
     title = {Aerodynamic characteristics of $\Lambda$-shaped wings at subsonic speeds of flight},
     journal = {Vestnik Moskovskogo universiteta. Matematika, mehanika},
     pages = {89--91},
     publisher = {mathdoc},
     number = {1},
     year = {1983},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/VMUMM_1983_1_a22/}
}
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V. I. Voronin. Aerodynamic characteristics of $\Lambda$-shaped wings at subsonic speeds of flight. Vestnik Moskovskogo universiteta. Matematika, mehanika, no. 1 (1983), pp. 89-91. http://geodesic.mathdoc.fr/item/VMUMM_1983_1_a22/