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NASA NTRS · Conference Paper

The NASA aircraft icing research program

Published 2013-08-29 From Legacy CDMS 2 authors
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Attribution

This is the abstract and citation. Full text lives at NASA NTRS — we link out rather than host. All credit to the authors and Legacy CDMS.

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

The objective of the NASA aircraft icing research program is to develop and make available to industry icing technology to support the needs and requirements for all-weather aircraft designs. Research is being done for both fixed wing and rotary wing applications. The NASA program emphasizes technology development in two areas, advanced ice protection concepts and icing simulation. Reviewed here are the computer code development/validation, icing wind tunnel testing, and icing flight testing efforts.

Authors

  • Shaw, Robert J. NASA Lewis Research Center
  • Reinmann, John J. NASA Lewis Research Center

Citation: Shaw, Robert J., Reinmann, John J. (2013). The NASA aircraft icing research program. Legacy CDMS. NASA NTRS ID 19920013291. https://ntrs.nasa.gov/citations/19920013291 ↗