Portal de Periódicos da CAPES

Suppressing a High-Frequency Instability with Varying Bands of White Noise

2014; American Institute of Aeronautics and Astronautics; Volume: 30; Issue: 4 Linguagem: Inglês

10.2514/1.b35232

1533-3876

John W. Bennewitz, Robert A. Frederick, David M. Lineberry,

Rocket and propulsion systems research

No AccessTechnical NoteSuppressing a High-Frequency Instability with Varying Bands of White NoiseJohn W. Bennewitz, Robert A. Frederick Jr. and David M. LineberryJohn W. BennewitzPropulsion Research Center, Johnson Research Center, University of Alabama in Huntsville, Huntsville, Alabama 35899*Graduate Research Assistant, Propulsion Research Center, Johnson Research Center, Room 107. Student Member AIAA.Search for more papers by this author, Robert A. Frederick Jr.Propulsion Research Center, Johnson Research Center, University of Alabama in Huntsville, Huntsville, Alabama 35899†Director, Propulsion Research Center, Technology Hall. Room S225; currently Professor, Mechanical and Aerospace Engineering. Associate Fellow AIAA.Search for more papers by this author and David M. LineberryPropulsion Research Center, Johnson Research Center, University of Alabama in Huntsville, Huntsville, Alabama 35899‡Research Engineer, Propulsion Research Center, Johnson Research Center, Room 101. Senior Member AIAA.Search for more papers by this authorPublished Online:1 Jul 2014https://doi.org/10.2514/1.B35232SectionsView Full TextPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Lubarsky E., Shcherbik D. and Zinn B. T., “Active Control of Combustion Oscillations by Non-Coherent Fuel Flow Modulation,” 9th AIAA/CEAS Aeronautics Conference and Exhibit, AIAA Paper 2003-3180, 2003. LinkGoogle Scholar[2] Bennewitz J. W. and Frederick R. A.,, “Overview of Combustion Instabilities in Liquid Rocket Engines—Coupling Mechanisms and Control Techniques,” 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 2013-4106, 2013. LinkGoogle Scholar[3] Bennewitz J. W., Lineberry D. M. and Frederick R. A.,, “Application of High Frequency Pressure Disturbances as a Control Mechanism for Liquid Rocket Engine Combustion Instabilities,” 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 2013-3853, 2013. Google Scholar[4] Byrd R. E. and Frederick R. A.,, “Instability Characteristics of a Gaseous-Oxygen/Methane Pentad Injector,” Journal of Propulsion and Power, Vol. 26, No. 4, 2010, pp. 689–695. doi:https://doi.org/10.2514/1.41434 JPPOEL 0748-4658 LinkGoogle Scholar Previous article Next article