Direct prediction of unstable waves in combustion chamber

W. S. Yoon, G. Y. Lee

Research output: Contribution to conferencePaper

Abstract

Aiming at a direct, also more realistic, prediction of unstable waves evolving in the combustion chamber, present paper introduces a new analytical method. Instability equations are freshly formulated, and solve the time-integrated ODE's for amplification factors to find the transients of pressure and velocity fluctuations. Present numerical approach requires no separate treatments for nonlinearities. Preliminary numerical experiments for unstable waves in quasi-onedimensional rocket combustor, show validity and applicability of present model, and promise for its practical use. Study for the complex models for physics, especially velocity- and pressure-coupled responses, and inclusion of multi dimensionality remains as future tasks.

Original languageEnglish
DOIs
Publication statusPublished - 2001
Event37th Joint Propulsion Conference and Exhibit 2001 - Salt Lake City, UT, United States
Duration: 2001 Jul 82001 Jul 11

Other

Other37th Joint Propulsion Conference and Exhibit 2001
CountryUnited States
CitySalt Lake City, UT
Period01/7/801/7/11

All Science Journal Classification (ASJC) codes

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

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    Yoon, W. S., & Lee, G. Y. (2001). Direct prediction of unstable waves in combustion chamber. Paper presented at 37th Joint Propulsion Conference and Exhibit 2001, Salt Lake City, UT, United States. https://doi.org/10.2514/6.2001-3848