This report discusses in detail the results obtained with devices for preventing the separation of the boundary layer. In order to give an idea of the order of magnitude of the positive and negative pressures involved, we made a diagram of them, as measured at 15 degrees angle of attack on the Gottigen profile 387. The pressure scale is graduated in terms of the dynamic pressure q, which enables the evaluation of the positive and negative pressures at all velocities.
The use of slots for increasing the lift of airplane wings
1931-08-01
Miscellaneous
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English
Use of slots for increasing lift of airplane wings
Engineering Index Backfile | 1931
|Use of slots for increasing lift of airplane wings
Engineering Index Backfile | 1931
|The use of slots for increasing the lift of airplane wings
TIBKAT | 1931
|Simple method for increasing lift of airplane wings by means of flaps
Engineering Index Backfile | 1933
|Application of slots and flaps to airplane wings in America
Engineering Index Backfile | 1933
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