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Vortex conception of rotor and mutual effect of screw/propellersA vortex theory of screw/propellers with variable circulation according to the blade and its azimuth is proposed, the problem is formulated and circulation is expanded in a Fourier series. Equations are given for inductive velocities in space for crews, including those with an infinitely large number of blades and expansion of the inductive velocity by blade azimuth of a second screw. Multiparameter improper integrals are given as a combination of elliptical integrals and elementary functions, and it is shown how to reduce elliptical integrals of the third kind with a complex parameter to integrals with a real parameter.
Document ID
19860012039
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Lepilkin, A. M.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-77979
NAS 1.15:77979
Report Number: NASA-TM-77979
Report Number: NAS 1.15:77979
Accession Number
86N21510
Funding Number(s)
CONTRACT_GRANT: NASW-4005
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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