作者: Griffin Y. Anderson , Daniel P. Bencze , Bobby W. Sanders
DOI:
关键词: Aerospace engineering 、 Scramjet 、 Engineering 、 Automotive engineering 、 Airframe 、 Thrust 、 Hypersonic speed 、 Ramjet 、 Propulsion 、 Combustor 、 Hypersonic flight
摘要: The feasibility of developing a hypersonic hydrogen-fueled airbreathing vehicle capable Mach 8 is examined. A modular dual-mode scramjet concept integrated with the airframe has been proposed. research involved in formation this design discussed. Particular attention given to studies concerned integration; evaluation inlets; and analysis viscous phenomena. injector combustor configurations engine, which designed operate as ramjet scramjet, are analyzed. engine thrust performance subscale modules was tested, positive results were obtained. Simulation testing full-size model being planned.