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A method of predicting flow rates required to achieve anti-icing performance with a porous leading edge ice protection systemA proposed method of analytically predicting the minimum fluid flow rate required to provide anti-ice protection with a porous leading edge system on a wing under a given set of flight conditions is presented. Results of the proposed method are compared with the actual results of an icing test of a real wing section in the NASA Lewis Icing Research Tunnel.
Document ID
19830011467
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kohlman, D. L. (Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1983
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
KU-FRL-464-5
NASA-CR-169996
NAS 1.26:169996
Report Number: KU-FRL-464-5
Report Number: NASA-CR-169996
Report Number: NAS 1.26:169996
Accession Number
83N19738
Funding Number(s)
CONTRACT_GRANT: NAG3-71
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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