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Wing profile design of the world championship sail plane SB 11A glider capable of climbing while circling in an updraft at low speed with a great mount of lift while gliding to the next updraft at high speed and with minimal altitude loss was designed. The wing profile design alleviates several problems and leaves no gap between wind and flap. A constant thickness flap eliminates the need for a flexible contour section which in turn reduces control effort. The conventional method of banking with ailerons is retained. Improved performance is demonstrated.
Document ID
19800022879
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Horstmann, K. H.
(NASA Headquarters Washington, DC United States)
Quast, A.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1980
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-75829
Report Number: NASA-TM-75829
Accession Number
80N31385
Funding Number(s)
CONTRACT_GRANT: NASW-3198
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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