Means for computational and experimental investigations of aeroelastic stability of highly-maneuverable missiles

Аuthors

Bykov A. V.

Toropov Machine-Building Design Bureau "Vimpel", 90, Volokolamskoe shosse, Moscow, 125424, Russia

e-mail: a.bikov@mail.ru

Abstract

Hardware and software means for computational and experimental aeroelasticity investigations of «air-to-air» class missiles, such as ground vibration tests, flutter computations, aeroservoelasticity investigations are discussed.

Keywords:

aeroelastic stability, flutter, firmware, GVT.