Spontaneous Longitudinal Combustion Instability in a Continuously-Variable Resonance Combustor
作者： Yen C. Yu , James C. Sisco , Stanford Rosen , Ajay Madhav , William E. Anderson
DOI: 10.2514/1.B34308
关键词: Combustor 、 Materials science 、 Resonance 、 Chamber pressure 、 Combustion chamber 、 Oscillation 、 Mechanics 、 Combustion 、 Injector 、 Rocket
摘要: … The experiment is designed to efficiently obtain stability data under variable resonance … between the variable-length oxidizer tube and the fixed-length combustion chamber, thereby …
sci-hub.se 参考文章(32)
D. T. Harrje, Liquid propellant rocket combustion instability ,(1972)
John William Strutt, The Explanation of certain Acoustical Phenomena Scientific Papers. pp. 348- 354 ,(2009) , 10.1017/CBO9780511703966.056
Sin-I Chemg, Luigi Crocco, Theory of Combustion Instability in Liquid Propellant Rocket Motors ,(1956)
Vigor Yang, William E Anderson, Liquid rocket engine combustion instability American Institute of Aeronautics and Astronautics. ,(1995) , 10.2514/4.866371
F. E. Culick, Paul Kuentzmann, Unsteady Motions in Combustion Chambers for Propulsion Systems ,(2006)
D. E. Soko, C. J. Morgan, Longitudinal instability limits with a variable length hydrogen-oxygen combustor. ,(1969)
James C. Sisco, Measurement and analysis of an unstable model rocket combustor Ph.D. Thesis. ,(2007)
Yen Ching Yu, Experimental and analytical investigations of longitudinal combustion instability in a continuously variable resonance combustor (CVRC) Ph.D. Thesis. ,(2009)
Yen Yu, Loral O'Hara, James Sisco, William Anderson, Experimental Study of High-Frequency Combustion Instability in a Continuously Variable Resonance Combustor (CVRC) 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. ,(2009) , 10.2514/6.2009-234
R. Smith, G. Xia, W. A. Anderson, C. L. Merkle, Computational Simulations of the Effect of Backstep Height on Nonpremixed Combustion Instability AIAA Journal. ,vol. 48, pp. 1857- 1868 ,(2010) , 10.2514/1.40385