This report is on the changes in forces on each wing of a biplane cellule when either the stagger or the gap is varied. Since each test was carried up to a 90 degree angle of attack, the results may be used in the study of stalled flight and of spinning as well as in the structural design of biplane wings.
Wind Tunnel Pressure Distribution Tests on a Series of Biplane Wing Models
1929-07-01
Miscellaneous
No indication
English