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CONDITIONS OF PHYSICAL MODELING AERODYNAMIC CHARACTERISTICS OF AIRCRAFT WITH CHASSIS HOVERCRAFT

The features of the physical modeling in the experimental determination of aerodynamics-cal tubes (WT) of low-velocity steady and unsteady aerodynamic characteristics at takeoff and landing of aircraft (LA) with the chassis air-cushion (ball screw) and in studies to determine the stability of equili...

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Autors principals: Yu. Yu. Merzlikin, A. A. Dolgopolov, V. G. Cipenko
Format: Artigo
Idioma:Russo
Publicat: Moscow State Technical University of Civil Aviation 2016-11-01
Col·lecció:Научный вестник МГТУ ГА
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Accés en línia:https://avia.mstuca.ru/jour/article/view/382
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