4/7/13    08:30 - 11:50 PP.06: Combustion Stability 1

ThM07 Room: Holiday Inn - Forum 10 Chair: Michael Oschwald CoChair: Changjin Lee Rapporteur: to be confirmed

Numerical simulation of the acoustical properties in rocket combustion chamber. R. Pongratz and D. Redmann Impact of Axial Gradients on Combustion Chamber Acoustics R. Kaess, S. Koeglmeier, R. Behr, B. Kniesner and T.  Sattelmayer Determination of the nozzle admittance in frequency domain for a generic test case M. Schulze, J. Gikadi and T. Sattelmayer Response Characterization of a LOX-GH2 Flame to Forced Acoustic Pressure Fluctuations T. Ramcke, M. Schmid and T. Sattelmayer On the Reflection, Transmission, Coupling and Damping of Non-Plane Acoustic Modes by Resonator Rings (*) A. Cárdenas Miranda and W. Polifke Stability behaviour of a cylindrical rocket engine combustion chamber operated with liquid hydrogen and liquid oxygen (*) S. Gröning, D. Suslov, M. Oschwald and T. Sattelmayer Cryogenic oxygen jet response to transverse acoustic excitation with 1T and 1L1T modes J.S. Hardi and M. Oschwald