01827–6119-T000.įirst International Symposium on Liquid Rocket Engine Instability (Proceedings) (1993) The Pennsylvania State University, January 18–20, 1993.Īubrey, N., Holmes, P., Lumley, J. This process is experimental and the keywords may be updated as the learning algorithm improves.Īnonymous (1967) “Engine Characteristics and Stability,” Chapter 4 of TRW document No. These keywords were added by machine and not by the authors. On that basis, a general framework can be constructed to serve both practical and theoretical purposes. In that context, the systems are distinguished chiefly by geometry and the kinds of propellants used. None of the propulsion systems are covered in great detail, but sufficiently to establish the fundamental point that while there are obvious practical differences among the systems, for understanding and treating combustion instabilities, much is to be gained by treating the various phenomena within a common framework. Virtually all of the material included here has appeared elsewhere, either in primary research reports or in reviews. The purpose of this paper is to give a broad overview of the field of combustion instabilities in propulsion systems.
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