Wind tunnel pressure distribution tests on a series of biplane wing models Part III: effects of charges in various combinations of stagger, gap, sweepback, and decalage Page: 2 of 30
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NSA Technical ibrry
3 1176 01431 9280
ERRATA
NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS.
TECHNICAL NOTE NO. 330.'
WIND TUNNEL PRESSURE DISTRIBUTION TESTS ON
A SERIES OF BIPLANE WING MODELS.
PART III. EFFECTS OF CHANGES IN VARIOUS COMBINATIONS
OF STAGGER, GAP, SWEEPBACK, AND DECALAGE.
On Figures 12, 13, 14, 16, 17, 18 and 19, after the word
"monorlane," insert "without sweepback."
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Knight, Montgomery & Noyes, Richard W. Wind tunnel pressure distribution tests on a series of biplane wing models Part III: effects of charges in various combinations of stagger, gap, sweepback, and decalage, report, December 1929; (https://digital.library.unt.edu/ark:/67531/metadc54019/m1/2/: accessed April 24, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.