Combustor performance enhancement through direct shear layer excitation
Open Access
- 1 October 1990
- journal article
- Published by Elsevier in Combustion and Flame
- Vol. 82 (1) , 75-92
- https://doi.org/10.1016/0010-2180(90)90079-7
Abstract
No abstract availableKeywords
This publication has 23 references indexed in Scilit:
- Vortex-driven acoustically coupled combustion instabilitiesJournal of Fluid Mechanics, 1987
- Longitudinal combustion instabilities in ramjet engines Identification of acoustic modesJournal of Propulsion and Power, 1986
- The plane turbulent shear layer with periodic excitationJournal of Fluid Mechanics, 1985
- The forced mixing layer between parallel streamsJournal of Fluid Mechanics, 1982
- Subharmonics and vortex merging in mixing layersJournal of Fluid Mechanics, 1982
- Mechanism of Instabilities in Turbulent Combustion Leading to FlashbackAIAA Journal, 1982
- Vortex pairing in a circular jet under controlled excitation. Part 1. General jet responseJournal of Fluid Mechanics, 1980
- Measurement of Vortex Frequencies in a Lean, Premixed Prevaporized Combustor†Combustion Science and Technology, 1979
- Structure of Turbulent Shear Flows: A New LookAIAA Journal, 1976
- The mechanism of interaction between a combustion region and acoustic resonatorActa Astronautica, 1976