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AEROHYDROMECHANIC THEORY OF WING IN A NONSTATIONARY FLOW (SELECTED PARTS)
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
A formula is obtained for the power of liquid pressure on a profile situated in nonstationary motion. A mathematical theory is offered of an arrangement, proposed for reducing the rate of landing of parachute loads.
Unedited rough draft trans. of mono. Teoreticheskaya i Prikladnaya Mekhanika. Sbornik Statei, v. 2, Moscow, 1962, p. 100-101, 611-622.