Pressure distribution on a slotted R.A.F. 31 airfoil in the variable density wind tunnel

Eastman N. Jacobs
naca-tn-308
Jun 1929


Measurements were made in the variable density wind tunnel to determine the pressure distribution over one section of a R.A.F. 31 airfoil with a leading edge slot fully open. To provide data for the study of scale effect on this type of airfoil, the tests were conducted with air densities of approximately one and twenty atmospheres.

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