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Propulsion integration for a hybrid propulsive-lift system

Authors :
Bowden, M. K
Renshaw, J. H
Sweet, H. S
Publication Year :
1974
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1974.

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.

Subjects

Subjects :
Aerodynamics

Details

Language :
English
Database :
NASA Technical Reports
Publication Type :
Report
Accession number :
edsnas.19740052252
Document Type :
Report