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NASA's rotorcraft icing research programThe objective of the NASA aircraft icing research program is to develop and make available icing technology to support the needs and requirements of industry for all weather aircraft designs. While a majority of the technology being developed is viewed to be generic (i.e., appropriate to all vehicle classes), vehicle specific emphasis is being placed on the helicopter due to its unique icing problems. In particular, some of the considerations for rotorcraft icing are indicated. The NASA icing research program emphasizes technology development in two key areas: ice protection concepts and icing simulation (analytical and experimental). The NASA research efforts related to rotorcraft icing in these two technology areas will be reviewed.
Document ID
19880007258
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Shaw, Robert J.
(NASA Lewis Research Center Cleveland, OH., United States)
Reinmann, John J.
(NASA Lewis Research Center Cleveland, OH., United States)
Miller, Thomas L.
(Sverdrup Technology, Inc. Cleveland, Ohio., United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1988
Publication Information
Publication: NASA, Washington, NASA(Army Rotorcraft Technology. Volume 2: Materials and Structures, Propulsion and Drive Systems, Flight Dynamics and Control, and Acoustics
Subject Category
Air Transportation And Safety
Accession Number
88N16641
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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