3/7/13    08:30 - 11:50
PP.32: Propellant Injection
WeM04
Room: Holiday Inn - Forum 6
Chair: Yu Daimon
CoChair: Dimitry Suslov
Rapporteur: to be confirmed
Temperature measurement of cryogenic nitrogen jets at supercritical pressure
H. Tani, S. Teramoto, T. Toki, S. Yoshida, K. Yamaguchi and K. Okamoto


Design, analysis and testing of a 3.5 kN coaxial pintle demonstrator engine
L. Souverein, P. Martin, A. Dahlhaus, C. Hoeglauer, V. Kaufmann, C. Maeding, K. Seeliger, E. Receveur and D. Fiot


Numerical simulations of mixing under supercritical pressures of a shear coaxial injector using a high-order method: effect of outer jet temperature
H. Terashima and M. Koshi


Large Eddy Simulation of Kerosene/LOx Supercritical Mixing Characteristics of a Swirl Injector using Various Cubic Equations of State
J.Y. Heo, K.J. Kim and H.G. Sung


Large-Eddy Simulation of Trans- and Supercritical Injection (*)
H. Müller, C.A. Niedermeier, M. Jarczyk, M. Pfitzner, S. Hickel and N.A. Adams


Numerical coupling strategies for the “separated-to-dispersed” transition within the liquid phase of cryogenic rocket engines
C. Le Touze, A. Murrone and E. Montreuil