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NASA's program on icing research and technologyNASA's program in aircraft icing research and technology is reviewed. The program relies heavily on computer codes and modern applied physics technology in seeking icing solutions on a finer scale than those offered in earlier programs. Three major goals of this program are to offer new approaches to ice protection, to improve the ability to model the response of an aircraft to an icing encounter, and to provide improved techniques and facilities for ground and flight testing. The following program elements are reviewed: (1) new approaches to ice protection; (2) numerical codes for deicer analysis; (3) measurement and prediction of ice accretion and its effect on aircraft and aircraft components; (4) special wind tunnel test techniques for rotorcraft icing; (5) improvements of icing wind tunnels and research aircraft; (6) ground de-icing fluids used in winter operation; (7) fundamental studies in icing; and (8) droplet sizing instruments for icing clouds.
Document ID
19900005746
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reinmann, John J.
(NASA Lewis Research Center Cleveland, OH, United States)
Shaw, Robert J.
(NASA Lewis Research Center Cleveland, OH, United States)
Ranaudo, Richard J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1989
Publication Information
Publication: AGARD, Flight in Adverse Environmental Conditions
Subject Category
Air Transportation And Safety
Accession Number
90N15062
Distribution Limits
Public
Copyright
Other
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