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.
Aerohydromechanic Theory of Wing in a Nonstationary Flow (Selected Parts)
1965
2 pages
Report
Keine Angabe
Englisch
Nonstationary flow about Wing-Aileron-Tab combination including aerodynamic balance
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