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NASA NTRS · 19740052252

Propulsion integration for a hybrid propulsive-lift system

Abstract

In a discussion of STOL vehicles with conventional high-lift devices, the need for efficient power-augmented lift systems is presented, and the implications of quiet operation are noted. The underlying philosophy of a promising hybrid lift system with major interactions between aerodynamic, thermodynamic, acoustic, and configuration design technologies is derived. The technique by which engine and airframe-related characteristics for this application may be matched in an optimum manner is described and illustrated by describing the features of a particular short-haul commercial STOL vehicle.

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BibTeXRIS

Bowden, M. K., Renshaw, J. H., Sweet, H. S.. 1974-04-01. Propulsion integration for a hybrid propulsive-lift system. https://ntrs.nasa.gov/citations/19740052252

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