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Aerodynamic Coefficients for an Oscillating Airfoil with Hinged Flap, with Tables for a Mach Number of 0.7
M. J. Turner
S. Rabinowitz
出版
National Advisory Committee for Aeronautics
, 1950
URL
http://books.google.com.hk/books?id=z26rtgAACAAJ&hl=&source=gbs_api
註釋
Dietze's method for the solution of Possio's integral equation is used to determine the chordwise distribution of lift on an oscillating airfoil with simple hinged flap in two-dimensional compressible flow (subsonic). Results of these calculations are used to prepare tables of aerodynamic coefficients for lift, pitching moment (referred to quarter-chord point), and flap hinge moment for a Mach number of 0.7; the motions considerd are vertical translation, airfoil rotation about a quarter-chord point, and rotation of the flap about its hinge line.
