SU549829A1

SU549829A1 - Training device for practical aerodynamics

Info

Publication number: SU549829A1
Application number: SU2165124A
Authority: SU
Inventors: Анатолий Михайлович Тарасенков; Юрий Петрович Потанин
Original assignee: Военно-Воздушная Инженерная Академия Им.Жуковского Н.Е.
Priority date: 1975-07-30
Filing date: 1975-07-30
Publication date: 1977-03-05

Description

к носику .модели, дл обратнойto the nose of the model, for the reverse

реакции К хвосту.K tail reaction.

Поворотом педалей // измен ют угол скольжени , а крен, при этом, действием под ,гфуж шенных т г образуетс : на консоль крыла iB сторону .скольжени - пр ма реакци , если точки креплени т г 14 .вынесены к носику, и на вторую консоль - обратна реакци , если эти точки вынесены .к хвосту модели. Максимальна глубина креиа уменьшаетс цри .приближении точек краплени т г 14 к .вертикальной плоскости, проход щей через поперечную ось модели, и достигает нулево1го значени в положении со.впадени точек с этой ПЛОСКОСТЬЮ.By turning the pedals, the slip angle is changed, and the roll, under the action under the pressure of the rifles, forms: on the wing console iB, the slide is a direct reaction if the attachment points of the slide 14 are extended to the spout, and to the second the console is the reverse reaction if these points are placed on the tail of the model. The maximum depth of the curve is reduced by approaching the points of droplet g to 14 to the vertical plane passing through the transverse axis of the model and reaches a zero value in the position of coincidence of points with this PLANE.

Предлагаемый учебный прибор обеспечивает на.гл дность три изучении влений пр мой и обратной реакции ino крену на скольжение летательных аппаратов.The proposed training device provides for three studies of the effects of direct and reverse ino roll reactions on aircraft gliding.

Claims

Invention Formula

A training device. On practical aerodynamics, containing a rack mounted on a frame, an airplane model with a rudder, fortified in a rack that can be rotated around two mutually perpendicular axes, and two rods, one end of each iKOTopbix attached to the wing of the model, This is due to the fact that, in order to be able to demonstrate the forward and backward response of the aircraft on roll to slip, it has a double-arm lever fixed to the frame, imitating aircraft pedals and connected to a model rzhn, mounted on the frame for longitudinal movement and located at its opposite ends, ichri eto.m thrust spring-loaded and formed with their free ends are attached to the rods.