AAAAAA

   
Results: 1-5 |
Results: 5

Authors: SCHLEY CA HAGEMANN G KRULLE G
Citation: Ca. Schley et al., TOWARDS AN OPTIMAL CONCEPT FOR NUMERICAL CODES SIMULATING THRUST CHAMBER PROCESSES IN HIGH-PRESSURE CHEMICAL PROPULSION SYSTEMS, Aerospace science and technology, 1(3), 1997, pp. 203-213

Authors: ROMMEL T HAGEMANN G SCHLEY CA KRULLE G MANSKI D
Citation: T. Rommel et al., PLUG NOZZLE FLOWFIELD ANALYSIS, Journal of propulsion and power, 13(5), 1997, pp. 629-634

Authors: HAGEMANN G KRULLE G HANNEMANN K
Citation: G. Hagemann et al., NUMERICAL FLOWFIELD ANALYSIS OF THE NEXT-GENERATION VULCAN NOZZLE, Journal of propulsion and power, 12(4), 1996, pp. 655-661

Authors: SCHLEY CA HAGEMANN G KRULLE G
Citation: Ca. Schley et al., TOWARDS AN OPTIMAL CONCEPT FOR NUMERICAL CODES SIMULATING THRUST CHAMBER PROCESSES IN HIGH-PRESSURE CHEMICAL PROPULSION SYSTEMS, Acta astronautica, 38(4-8), 1996, pp. 427-436

Authors: MAYER W KRULLE G
Citation: W. Mayer et G. Krulle, ROCKET ENGINE COAXIAL INJECTOR LIQUID-GAS INTERFACE FLOW PHENOMENA, Journal of propulsion and power, 11(3), 1995, pp. 513-518
Risultati: 1-5 |