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Theoretical and experimental investigation of vortex breakdownThe slender-vortex approximation was analyzed for incompressible and compressible flow. First the equations of motion were reduced in an order of magnitude analysis. Then compatibility conditions were formulated for the inflow conditions. Thereafter finite-difference-solutions were constructed for incompressible and compressible flow. Finally it was shown that these solutions can be used to describe the flow in slender vortices. The analysis of the breakdown process must, however, be excluded, since its upstream influence cannot be predicted with the slender vortex approximation. The investigaton of this problem is left for future work.
Document ID
19860022058
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Krause, E.
(Technische Hochschule Aachen, Germany)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-176853
NAS 1.26:176853
Report Number: NASA-CR-176853
Report Number: NAS 1.26:176853
Accession Number
86N31530
Funding Number(s)
CONTRACT_GRANT: NAGW-816
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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