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Introduction to the arcopter arc wing and the Bertelsen effect for positive pitch stability and controlA brief report, offered on a wing design, new in geometry, construction, and flight characteristics. Preliminary wind tunnel data on a three-dimensional model was well as some full-scale man-carrying test results are included. There are photos of all phases of the experiments and some figures which serve to illustrate the Bertelsen Effect, a unique focus of aerodynamic forces in the arc wing system which allows the attainment of high lift coefficients with the maintenance of pitch stability and control.
Document ID
19790015724
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bertelsen, W. D.
(Bertelsen Mfg. Co., Inc. Neponset, IL, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: NASA. Langley Res. Center The Sci. and Technol. of Low Speed and Motorless Flight, Pt. 1
Subject Category
Aircraft Stability And Control
Accession Number
79N23895
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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