Carrying out field and flight tests to verify the influence of moment-inertia layout parameters to the aircraft form

Аuthors

Dolgov O. S.^*, Sosedko A. A.^**

Kompany “ACA” , 10/1, M. Jalil St.,115573, Russia

*e-mail: dolgov@mai.ru
**e-mail: info@asa-2.ru

Abstract

The paper describes alternative variants of tandem scheme aircrafts moment-inertia forms. Analyze the effect of moment-inertia characteristics changing to the formation of aircraft. The axial moments of inertia values for the existing aircraft was determined experimentally on the basis of field and flight tests, as well as using specialized software «МИФ».

Keywords:

moment of inertia; layout; field and flight tests; aircraft form.