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Evaluation of a surface panel method coupled with several boundary layer analysesThree boundary layer models are interacted with an inviscid panel method to evaluate their capabilities to predict aerodynamic performance characteristics. These boundary layer models include two two-dimensional boundary layer models and one three-dimensional boundary layer model. Previously reported discrepancies between the transpiration and surface displacement inviscid boundary layer simulations are discussed and resolved. Results from each of the models are compared with experimental data.
Document ID
19830054821
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kjelgaard, S. O.
(NASA Langley Research Center Low-Speed Aerodynamics Div., Analytical Methods Branch, Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 83-0011
Accession Number
83A36039
Distribution Limits
Public
Copyright
Other

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