Measurement of pressures in variable-density tunnel at 54 orifices distributed over midspan section of 5- by 30-in. rectangular model of airfoil at 17 angles of attack ranging from 20 to 30° at Reynolds Number of approximately 3,000,000 for studying deviations of results of potential-flow theory from measured results. (10¢)
Calculated and measured pressure distributions over midspan section of N.A.C.A. 4412 airfoil
Nat Advisory Committee Aeronautics -- Report
1936
16 pages
Report
English
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Pressure distribution over N.A.C.A. 23012 airfoil with N.A.C.A. 23012 external-airfoil flap
Engineering Index Backfile | 1938
|Pressure distribution over N.A.C.A. 23012 airfoil with N.A.C.A. 23012 external-airfoil flap
Engineering Index Backfile | 1938
|Pressure distribution over N.A.C.A. 23012 airfoil with N.A.C.A. 23012 external-airfoil flap
Engineering Index Backfile | 1938
|