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

Аuthors

Pravidlo M. N.

Toropov Machine-Building Design Bureau "Vimpel", 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

Download