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Prediction of the lift and moment on a slender cylinder-segment wing-body combination

Published online by Cambridge University Press:  04 July 2016

K. R. Crowell  and
C. T. Crowe
K. R. Crowell
Affiliation:
Department of Mechanical Engineering, Washington State University
C. T. Crowe
Affiliation:
Department of Mechanical Engineering, Washington State University
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Extract

The design of a vehicle with cruise capability which can be packaged in a volume limited space, such as a cylindrical tube, centres around the problem of folding the lifting and control surfaces in such a manner that their deployment is simple and reliable. Several folding schemes are illustrated in Fig. 1. A wing fabricated of a flexible material and suspended by lines from the fuselage (parawing, Fig. 1a) can be folded to occupy only a small volume. These wings, however, are difficult to deploy at high forward speeds and have characteristically poor lift/ drag ratios unsuitable for high performance cruise capability. Another concept which allows storing the wing in a volume-limited space is the “scissor” wing (Fig. 1b) which, when deployed, swings out from a cavity in the fuselage.

Type
Technical notes
Information
The Aeronautical Journal , Volume 77 , Issue 750 , June 1973 , pp. 295 - 298
Copyright
Copyright © Royal Aeronautical Society 1977 

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