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Ambiguity of solution for triple configurations of stationary shocks with negative reflection angle

  • Published:2021-02 Issue: Volume:179 Page:382-390
  • ISSN:0094-5765
  • Container-title:Acta Astronautica
  • language:en
  • Short-container-title:Acta Astronautica

Author:

Chernyshov M.V.,Kapralova A.S.,Savelova K.E.

Funder

Ministry of Science and Higher Education of the Russian Federation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

1. Gas Dynamics of Outflow Processes;Dulov,1984

2. Numerical investigation on a new concept of shock vector control nozzle;Shi;J. Eng. Gas Turbines Power,2019

3. Design and wall fluid parameters evaluatiob of the dual-bell nozzle;Hamitouche;Int. J. Eng. Res. Technol.,2019

4. Over-expanded separation transitions of single expansion ramp nozzle in the accelerationg and decelerating processes;Yu;Aero. Sci. Technol.,2020

5. Shock Wave Reflection Phenomena;Ben-Dor,2007

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1. Research of an oblique detonation wave in a limited area;Acta Astronautica;2024-02

2. Method of calculation of satellite flow parameters behind the point of Mach reflection;E3S Web of Conferences;2024

3. Analytical study of the possibilities of controlling the parameters of shocks in supersonic flow around gas-permeable bodies;XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION;2023

4. Type IV shock interaction with a two-branch structured transonic jet;Journal of Fluid Mechanics;2022-05-06

5. Triple Configurations of Steady and Propagating Shocks;Russian Aeronautics;2022-04
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