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On the Theory of Oscillating Wings in Sonic Flow
Author(s) -
Dragoş L.
Publication year - 1988
Publication title -
zamm ‐ journal of applied mathematics and mechanics / zeitschrift für angewandte mathematik und mechanik
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.449
H-Index - 51
eISSN - 1521-4001
pISSN - 0044-2267
DOI - 10.1002/zamm.19880680819
Subject(s) - wing , flow (mathematics) , section (typography) , physics , aspect ratio (aeronautics) , classical mechanics , mathematics , mechanics , mathematical analysis , computer science , thermodynamics , optoelectronics , operating system
Using the fundamental solution method developed in [1], [2], in this paper a novel theory of the oscillating wing in sonic flow is given. An integral equation is obtained which has the advantage that its exact solutions are known in certain cases. One of these cases concerns the rectangular wing of low aspect ratio and is dealt with in the last section.