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- W2049914021 abstract "In the linearized formulation of the oscillating-surf ace problem, singularities in the lift distribution occur at subsonic leading edges, at control surface leading edges, and in general wherever the up wash prescribed by the wing deformations is discontinuous. These singularities are examined by use of the method of matched asymptotic expansions. It is shown that for a known discontinuity in upwash (as in the case of the control surface) the form, as well as the strength, of the singularity are determined uniquely. For subsonic leading edges only the form, but not the strength, of the singularity can be determined. A discussion is also given of the proper shape of the loading functions near side edges. Nomenclature b = reference length (root semi chord) Cp = pressure coefficient k = reduced frequency, ub/Um M = Mach number of freestream MN = M cos A, Mach number normal to edge p — pressure amplitude, Cp = peikt t = time Um = freestream velocity w = amplitude of prescribed upwash on the wing X) y} z = Cartesian coordinates with x in the freestream and in the span wise direction xc = location of control-surfa ce leading edge and hinge Xj y, z = stretched variables" @default.
- W2049914021 created "2016-06-24" @default.
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- W2049914021 date "1968-02-01" @default.
- W2049914021 modified "2023-09-25" @default.
- W2049914021 title "Pressure-loading functions for oscillating wings with control surfaces." @default.
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- W2049914021 doi "https://doi.org/10.2514/3.4500" @default.
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