Experimental and numerical SCRAMJET research

A propulsion systems for flight mach numbers > 8 is the so called SCRAMJET, an aerothermodynamic duct flight propulsion system including a supersonic combustion flow. The Institute for Flight Propulsion investigates different systems for fuel injection. Investigation are performed in modell combustion chamber using modern optical laser measurement systems. Results are used to develope a designing software, which allows to predict the performance of a whole SCRAMJET.

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