Numerical results for coefficients of system where aileron hinge axis coincides with nose of aileron; complete set of 5 complex coefficients is given for Mach numbers 0, 0.35, 0.50, 0.60, 0.70, 0. 80, reduced frequency being equal to 0 (0.1) 1.0 and chord ratio equal to 0 (0.02) 0.1 (0.05) 0.3.
Tables of aerodynamic aileron-coefficients for oscillating wing-aileron system in subsonic, compressible flow
Amsterdam Nationaal Luchtvaartlaboratorium (Nat Aeronautical Research Inst) -- Report
1954
21 pages
Report
English
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Tables of wing-aileron coefficients of oscillating air forces for two-dimensional supersonic flow
Engineering Index Backfile | 1950
|Engineering Index Backfile | 1956
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