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


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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.

Sobre autores

L. Bykov

Moscow Aviation Institute (National Research University)

Autor responsável pela correspondência
Email: bykov@mai.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993

O. Pashkov

Moscow Aviation Institute (National Research University)

Email: bykov@mai.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993

M. Pravidlo

Toropov State Machine Building Design Bureau “Vympel”

Email: bykov@mai.ru
Rússia, Volokolamskoe sh. 90, Moscow, 125424

V. Tishkov

Moscow Aviation Institute (National Research University)

Email: bykov@mai.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993

D. Yanyshev

Moscow Aviation Institute (National Research University)

Email: bykov@mai.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993

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