On “new methodologies of processing” of results calculated for rotating detonation engines and of results of force measure-ments for ramjet models tested in super-sonic test benches
A.N. Kraiko
Baranov Central Institute of Aviation Motors, Moscow, Russia
Keywords: rotating detonation engine (RDE), forces measured in “hot” and “cold” runs, model in a supersonic test bench, effective thrust
Abstract
It is shown that the “new methodologies” of processing and using results calculated for rotating detonation engines, as well as those of recent measurement of forces acting on the models of ramjet (rotorless) models in “hot” and “cold” runs in supersonic test benches, which are developed and promoted by S.M. Frolov and V.I Zvegintsev with their colleagues, are incorrect.
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