05 - Propulsion
RAMJET/SCRAMJET TEST BENCH WITH CAVITY INJECTION OF HYDROGEN
F. Strauss¹, T. Nilsson, Lund University, Sweden; K. Manassis¹; ¹German Aerospace Center DLR, Germany
In this work we study a small ramjet combustor with cavity injection of hydrogen. The work is embedded within the MDO and Regulations for Low-boom and Environmentally Sustainable Supersonic Aviation (More&Less) project (workpackage WP4) and compares two example cases of experimental combustion data for gaseous hydrogen with CFD simulated data for those cases. Includes an outlook on further data.