NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Rime-, mixed- and glaze-ice evaluations of three scaling lawsThis report presents the results of tests at NASA Lewis to evaluate three icing scaling relationships or 'laws' for an unheated model. The laws were LWC x time = constant, one proposed by a Swedish-Russian group and one used at ONERA in France. Icing tests were performed in the NASA Lewis Icing Research Tunnel (IRT) with cylinders ranging from 2.5- to 15.2-cm diameter. Reference conditions were chosen to provide rime, mixed and glaze ice. Scaled conditions were tested for several scenarios of size and velocity scaling, and the resulting ice shapes compared. For rime-ice conditions, all three of the scaling laws provided scaled ice shapes which closely matched reference ice shapes. For mixed ice and for glaze ice none of the scaling laws produced consistently good simulation of the reference ice shapes. Explanations for the observed results are proposed, and scaling issues requiring further study are identified.
Document ID
19940019574
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, David N.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Air Transportation And Safety
Report/Patent Number
NAS 1.15:106461
NASA-TM-106461
E-8323
AIAA PAPER 94-0718
Report Number: NAS 1.15:106461
Report Number: NASA-TM-106461
Report Number: E-8323
Report Number: AIAA PAPER 94-0718
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 10, 1994
End Date: January 13, 1994
Sponsors: AIAA
Accession Number
94N24047
Funding Number(s)
PROJECT: RTOP 505-68-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available