Examination of the improved model for the unsteady combustion around hypersonic projectiles

Akiko Matsuo, Kozo Fujii

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

Row features of the unsteady shock-induced combustion around projectiles are studied. The analysis is carried out with the numerical simulation using finite difference method. The large-disturbance regime unsteady combustion with the low frequency and high amplitude oscillation is investigated by a series of simulations considering the oxygen-hydrogen combustion mechanism under the same condition as the experiment. The time-evolving flow field is obtained in the simulation result, and the mechanism of the unsteady phenomenon is investigated. The mechanism on the stagnation streamline agrees with our previously proposed model using the simplified chemical reaction model. Factors for the large-disturbance regime unsteady combustion were detected in each computation. Some of new factors; self-enforced explotion and secondary explosion, arc detected and an improved model is proposed.

Original languageEnglish
Title of host publication31st Joint Propulsion Conference and Exhibit
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9780000000002
Publication statusPublished - 1995
Event31st Joint Propulsion Conference and Exhibit, 1995 - San Diego, United States
Duration: 1995 Jul 101995 Jul 12

Other

Other31st Joint Propulsion Conference and Exhibit, 1995
CountryUnited States
CitySan Diego
Period95/7/1095/7/12

ASJC Scopus subject areas

  • Energy Engineering and Power Technology
  • Electrical and Electronic Engineering
  • Mechanical Engineering
  • Control and Systems Engineering
  • Aerospace Engineering

Fingerprint Dive into the research topics of 'Examination of the improved model for the unsteady combustion around hypersonic projectiles'. Together they form a unique fingerprint.

  • Cite this

    Matsuo, A., & Fujii, K. (1995). Examination of the improved model for the unsteady combustion around hypersonic projectiles. In 31st Joint Propulsion Conference and Exhibit [AlAA 95-2565] American Institute of Aeronautics and Astronautics Inc, AIAA.