Experimental investigations on liquid film cooling in a GOX/ kerosene rocket combustion chamber.
C. Kirchberger, G. Schlieben and O.J. Haidn
Transfer of an analytical transpiration cooling model to the cooling analysis of rocket combustion chambers made of ceramic matrix composites (*)
M. Selzer, H. Hald, A. Herbertz, S. Schweikert and J. von Wolfersdorf
Radiative Heat Transfer Analysis in Modern Rocket Combustion Chambers
F. Goebel, B. Kniesner, M. Frey, O. Knab and C. Mundt
Evolution of Cooling-Channel Properties for Varying Aspect Ratio
M. Pizzarelli, F. Nasuti and M. Onofri
Numerical simulation of transpiration cooling through porous media
W. Dahmen, V. Gerber, T. Gotzen and S. Müller
Transient Fluid-Structure Interaction Analysis of a Cooled Rocket Thrust Chamber Based on Three Coupling Domains(*)
D. Kowollik, M. Haupt and P. Horst
Simulation of liquid, transcritical and gaseous cooling films
C. Höglauer, B. Kniesner, O. Knab, G. Schlieben and O.J. Haidn
Consideration of wall roughness effects in the prediction of heat transfer in rocket combustion chambers
B. Kniesner, M. Frey and O. Knab
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