PIV at a supersonic ramjet combustor

von Oschwald, M.
Veröffentlicht 1993

Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber

von Armbruster, W.
Veröffentlicht in International Symposium on Combustion (38. : 2021 : Adelaide) [38th International Symposium on Combustion] ; 10/11 (2021)

Measuring the velocity field of a shear-coaxial, cryogenic flame in a high-pressure rocket thrust chamber

von Son, M.
Veröffentlicht in International Symposium on Combustion (38. : 2021 : Adelaide) [38th International Symposium on Combustion] ; 5/11 (2021)

Experimental and numerical study of transcritical oxygen-hydrogen rocket flame response to transverse acoustic excitation

von Beinke, S. K.
Veröffentlicht in International Symposium on Combustion (38. : 2021 : Adelaide) [38th International Symposium on Combustion] ; 10/11 (2021)