No 325: Effects of changes in decalage; dihedral, sweepback, and overhang upon biplane wings are discussed; data obtained from pressure distribution tests made in atmospheric wind tunnel; way in which loadings on wings are effected by changes shows that results may be used in study of stalled flight and spinning and 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
6 pages
36 Supp. Figs.
Article (Journal)
English
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Engineering Index Backfile | 1929
|Wind tunnel pressure distribution tests on series of biplane wing models
Engineering Index Backfile | 1929
|