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Aircraft Vortex Wake Dynamics TsAGI, Moscow

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Gaifullin, A. M., author.
Conference Name:
World Aviation Congress & Exposition (1996-10-22 : Los Angeles, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1996
Summary:
The work deals with the problem on aircraft vortex wake behavior in steady-flow formulation. Further approximations of slender-body theory are constructed with the aid of asymptotic methods. The mathematical approach proposed performs to calculate the aircraft wake up to breakdown. The nontrivial analytic solutions for the problem of motion of one and two vortex filaments with circular cross-section are obtained
Notes:
Vendor supplied data
Publisher Number:
965547
Access Restriction:
Restricted for use by site license

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