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Effect of flap deflection on the lift coefficient of wings operating in a biplane configuration

Author
Stasiak, J.
Published
Nov 1, 1977.
Physical Description
1 electronic document
Online Version

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Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Biplane models with a lift flap were tested in a wind tunnel to study the effect of flap deflection on the aerodynamic coefficient of the biplane as well as of the individual wings. Optimization of the position flap was carried out, and the effect of changes in the chord length of the lower wing was determined for the aerodynamic structure of a biplane with a lift flap on the upper wing.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19780003060.
Accession ID: 78N11003.
NASA-TM-75059.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15730738