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.
Pressure Distribution on a Slotted R.A.F. 31 Airfoil in the Variable Density Wind Tunnel
1929-06-01
Miscellaneous
No indication
English
Pressure distribution on a slotted R.A.F. 31 airfoil in the variable density wind tunnel
Engineering Index Backfile | 1929
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