Inlet Channel for a Ducted Fan Propulsion System of a Light Aircraft release_6utn47aucvgsloinwgth6yosbm

by E. Ritschl, R. Theiner, D. Hanus

Published in Acta Polytechnica by CTU Central Library.

2003   Volume 43

Abstract

So-called "cold-jet" propulsion units consist of a piston engine, a blower and the necessary air duct. Till now, all attempts to utilize "cold-jet" propulsion units to maintain the thrust of an airplane have been unsuccessful. Analysis has shown that the main difficulty is the deformation of the flow field at the entry to the blower [1].
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