Numerical modeling on dynamic process of injection in supersonic part of the nozzle

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Abstract

The object of the study is the dynamic process of the impulsed jet injection into a supersonic flow in relation to the creation of control efforts. Basing on data from field experiment the study validates turbulence models and grid convergence.

About the authors

M. S. Yakovchuk

Baltic State Technical University named after D.F. Ustinov, St. Petersburg

Author for correspondence.
Email: mihailyakovchuk@gmail.com

Postgraduate Student

Russian Federation

References

  1. Органы управления вектором тяги твёрдотопливных ракет: расчёт, конструктивные особенности, эксперимент [Текст] / [Р.В. Антонов и др.]. Москва-Ижевск: НИЦ «Регулярная и хаотическая динамика», 2006. - 552 с.
  2. Аэродинамика отрывных течений [Текст] / [Н.Ф. Краснов и др.].- М.: Высш. шк., 1988. - 351 с.
  3. Spaid, F.W. A Study of the Interaction of Gaseous Jets from Transverse Slots with Supersonic External Flows [Text] / F.W. Spaid, E.E. Zucoski AIAA Journal Vol. 6, No 2, 1968.

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