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Wind tunnel pressure distribution tests on a series of biplane wing models Part II : effects of changes in decalage, dihedral, sweepback and overhangThis preliminary report furnishes information on the changes in the forces on each wing of a biplane cellule when the decalage, dihedral, sweepback and overhang are separately varied. The data were obtained from pressure distribution tests made in the Atmospheric Wind Tunnel of the Langley Memorial Aeronautical Laboratory. Since each test was carried up to 90 degree angle of attack, the results may be used in the study of stalled flight and of spinning and in the structural design of biplane wings.
Document ID
19930081102
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Knight, Montgomery
Noyes, Richard W
Date Acquired
September 6, 2013
Publication Date
October 1, 1929
Report/Patent Number
NACA-TN-325
Accession Number
93R10392
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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