Tables of multhopp and other functions for use in lifting-line and lifting-plane theory

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dc.contributor.author V. M. Falkner en_US
dc.contributor.author E. J. Watson en_US
dc.date.accessioned 2014-10-21T15:51:31Z
dc.date.available 2014-10-21T15:51:31Z
dc.date.issued 1948 en_US
dc.identifier.other ARC/R&M-2593 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3088
dc.description.abstract The report gives the derivation and computed tables of two classes of functions suitable for the solution of problems of spanwise aerodynamic loading of wings either by lifting-line or lifting-plane theory. The functions are based on lifting-line theory, but, by a consideration of the connection between lifting-line and lifting-plane theory through the application of I~nnk's stagger theorem to the calculation of induced drag, it is deduced that the functions must be equally suitable for lifting-plane theory. The first range of functions, called Multhopp or M functions, is associated with discontinuities of induced downwash, while the second, called P functions because of the polygonal representation of induced downwash, is connected with discontinuities in rate of change of induced downwash. Examples are given of the combination of functions to produce given curves of induced downwash, and evidence of the close relation between the results for a continuous and stepped downwash curve suggests that the functions tabulated will be sufficient to cover almost any problem in wing loading. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title Tables of multhopp and other functions for use in lifting-line and lifting-plane theory en_US


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