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

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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):

AERODYNAMICS

Collection:

NASA Technical Reports Server (NTRS) Collection.

Note:

Document ID: 19780003060.
Accession ID: 78N11003.
NASA-TM-75059.

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