Dietze's method for solution of Possio's integral equation used to determine chordwise distribution of lift on oscillating airfoil with simple hinged flap in two-dimensional compressible flow (subsonic); results of these calculations used to prepare tables of aerodynamic coefficients for lift, pitching moment and flap hinge moment for Mach number of 0.7.
Aerodynamic coefficients for oscillating airfoil with hinged flap, with tables for Mach number of 0.7
Nat Advisory Committee Aeronautics -- Tech Note
1950
46 pages
Tables, Graphs
Report
English
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