This report gives the results of wind-tunnel tests with a seaplane model as a contribution to the solution of the aerodynamic problems. In the tests it was assumed that the seaplane rested motionless on the water and was exposed, in various positions with respect to the supposedly flat surface of the water, to a uniform air current 0 to 360 degrees.
Aerodynamic Forces and Moments of a Seaplane on the Water
1933-11-01
Miscellaneous
No indication
English
Aerodynamic forces and moments of seaplane on water
Engineering Index Backfile | 1933
|Aerodynamic forces and moments of a seaplane on the water
TIBKAT | 1933
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