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The joined wing - An overviewThe joined wing is a new type of aircraft configuration which employs tandem wings arranged to form diamond shapes in plan view and front view. Wind-tunnel tests and finite-element structural analyses have shown that the joined wing provides the following advantages over a comparable wing-plus-tail system; lighter weight and higher stiffness, higher span-efficiency factor, higher trimmed maximum lift coefficient, lower wave drag, plus built-in direct lift and direct sideforce control capability. A summary is given of research performed on the joined wing. Calculated joined wing weights are correlated with geometric parameters to provide simple weight estimation methods. The results of low-speed and transonic wind-tunnel tests are summarized, and guidelines for design of joined-wing aircraft are given. Some example joined-wing designs are presented and related configurations having connected wings are reviewed.
Document ID
19850037475
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wolkovitch, J.
(ACA Industries, Inc. Torrance, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 85-0274
Accession Number
85A19626
Funding Number(s)
CONTRACT_GRANT: N00014-79-C-0953
CONTRACT_GRANT: N00014-82-C-0607
CONTRACT_GRANT: NAS2-11725
CONTRACT_GRANT: NAS2-11255
Distribution Limits
Public
Copyright
Other

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