NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Progress toward the development of an aircraft icing analysis capabilityAn overview of the NASA efforts to develop an aircraft icing analysis capability is presented. Discussions are included of the overall and long term objectives of the program as well as current capabilities and limitations of the various computer codes being developed. Descriptions are given of codes being developed to analyze two and three dimensional trajectories of water droplets, airfoil ice accretion, aerodynamic performance degradation of components and complete aircraft configurations, electrothermal deicer, and fluid freezing point depressant deicer. The need for bench mark and verification data to support the code development is also discussed.
Document ID
19840012422
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shaw, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-83562
E-1941
NAS 1.15:83562
Meeting Information
Meeting: Aerospace Sci. Meeting
Location: Reno, NV
Country: United States
Start Date: January 9, 1984
End Date: January 12, 1984
Sponsors: AIAA
Accession Number
84N20490
Funding Number(s)
PROJECT: RTOP 505-43-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available