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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Bibliographic Details
Main Authors: Yu. Yu. Merzlikin, A. A. Dolgopolov, V. G. Cipenko
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-11-01
Series:Научный вестник МГТУ ГА
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Online Access:https://avia.mstuca.ru/jour/article/view/382
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