On method of identification aerodynamic interference characteristics, during flight test data analysis

Aviation technics and technology


Аuthors

Pravidlo M. N.

State Machine Building Design Bureau «Vympel» by name I.I. Toropov, 90, Volokolamskoe shosse, Moscow, 125424, Russia

Abstract

In this article are discussed methods of flight test results evaluation, allowing identification of aircraft-carrier and missile aerodynamic interference characteristics for correction of mathematical model of missile separation aerodynamic.

Keywords:

launch system; aviation guided missile; aircraft-carrier; aerodynamic interference; aviation ejection launcher; telemetric records filtering; inverse problem solving


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