Thermo-acoustic stability of a helicopter gas turbine combustor using Large Eddy Simulation.

Autor: Boudier, G.1, Lamarque, N.1, Staffelbach, G.1, Gicquel, L. Y. M.1 lgicquel@cerfacs.fr, Poinsot, T.2
Zdroj: International Journal of Aeroacoustics. Jan2009, Vol. 8 Issue 1/2, p69-93. 25p. 11 Diagrams, 3 Graphs.
Databáze: Academic Search Ultimate