Calculation of Lifting Forces on Oscillating Wings
Author | : Valter J. E. Stark |
Publisher | : |
Total Pages | : 32 |
Release | : 1964 |
Genre | : Airplane wings |
ISBN | : |
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Author | : Valter J. E. Stark |
Publisher | : |
Total Pages | : 32 |
Release | : 1964 |
Genre | : Airplane wings |
ISBN | : |
Author | : Valter J. E. Stark |
Publisher | : |
Total Pages | : 23 |
Release | : 1964 |
Genre | : |
ISBN | : |
Author | : Aeronautical Research Council (Great Britain) |
Publisher | : |
Total Pages | : 43 |
Release | : 1966 |
Genre | : |
ISBN | : |
Author | : G. Z. Harris |
Publisher | : |
Total Pages | : 43 |
Release | : 1967 |
Genre | : Aerodynamic load |
ISBN | : |
Author | : G. Z. Harris |
Publisher | : |
Total Pages | : 43 |
Release | : 1965 |
Genre | : |
ISBN | : |
Author | : S. Y. Ruo |
Publisher | : |
Total Pages | : 60 |
Release | : 1975 |
Genre | : Aerodynamics, Transonic |
ISBN | : |
An analytical approach is presented to account for some of the nonlinear characteristics of the transonic flow equation for finite thickness wings undergoing harmonic oscillation at sonic flight speed in an inviscid, shock-free fluid. The thickness effect is accounted for in the analysis through use of the steady local Mach number distribution over the wing at its mean position by employing the local linearization concept and a coordinate transformation. Computed results are compared with that of the linearized theory and experiments. Based on the local linearization concept, an alternate formulation avoiding the limitations of the coordinate transformation method is presented.
Author | : Netherlands. National Luchtvaart-Laboratorium |
Publisher | : |
Total Pages | : |
Release | : 1956 |
Genre | : |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 32 |
Release | : 1959 |
Genre | : |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 32 |
Release | : 1959 |
Genre | : Aerodynamics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 76 |
Release | : 1962 |
Genre | : Aerodynamics |
ISBN | : |