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.
@article{VMUMM_1983_1_a22,
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},
year = {1983},
number = {1},
language = {ru},
url = {http://geodesic.mathdoc.fr/item/VMUMM_1983_1_a22/}
}
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/