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Russian Aeronautics

, Volume 61, Issue 2, pp 194–200 | Cite as

Numerical Simulation of Detachment Dynamics of a Payload from the Parent Aircraft

  • L. V. BykovEmail author
  • O. A. Pashkov
  • M. N. Pravidlo
  • V. V. Tishkov
  • D. S. Yanyshev
Flight Dynamics and Control of Flight Vehicles
  • 6 Downloads

Abstract

This paper presents the numerical simulation of detachment dynamics of a payload from its parent aircraft. The simulation allowed obtaining the free motion parameters of the payload taking into account its mass and momentum characteristics, aerodynamic forces and moments as well as gravity.

Keywords

parent aircraft payload gas dynamics equations mesh model computational fluid dynamics aerodynamic performance 

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Copyright information

© Allerton Press, Inc. 2018

Authors and Affiliations

  • L. V. Bykov
    • 1
    Email author
  • O. A. Pashkov
    • 1
  • M. N. Pravidlo
    • 2
  • V. V. Tishkov
    • 1
  • D. S. Yanyshev
    • 1
  1. 1.Moscow Aviation Institute (National Research University)MoscowRussia
  2. 2.Toropov State Machine Building Design Bureau “Vympel”MoscowRussia

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