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CFD Method for Aircraft Skid Performance Including Wear and Heat Transfer Hawker Beechcraft Corporation

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Carroll, George W., author.
Conference Name:
Wichita Aviation Technology Congress & Exhibition (2008-08-19 : Wichita, Kansas, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 2008
Summary:
A CFD method for predicting wear and heat transfer for an aircraft skid is described. It uses a finite volume method with a moving grid to account for wear. Therefore the skid material flows through the grid. The interface between the skid and runway is modeled empirically and is based on test data. A calculation for a simple skid is presented. The code is written in Mathematica which runs quickly and therefore is useful for experimenting with physical models and conducting trade studies
Notes:
Vendor supplied data
Publisher Number:
2008-01-2249
Access Restriction:
Restricted for use by site license

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