No 310: Effects of changes in forces on each wing of biplane cellule when either stagger or gap is varied are shown in data obtained from distribution tests made in atmospheric wind tunnel; since each test was carried up to 90-deg. angle of attack, results may be used in study of stalled flight and of spinning as well as in structural design of biplane wings.
Wind tunnel pressure distribution tests on a series of biplane wing models; effects of changes in stagger and gap
Nat. Advisory Committee Aeronautics -- Tech. Note
1929
13 pages
23 Figs.
Report
Englisch
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Engineering Index Backfile | 1929
|Wind tunnel pressure distribution tests on series of biplane wing models
Engineering Index Backfile | 1929
|