Computational Simulation of Large Droplet Icing

Wright, William B.; Potapczuk, Mark G.

doi:10.21949/1403450

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ROSA P serves as an archival repository of USDOT-published products including scientific findings, journal articles, guidelines, recommendations, or other information authored or co-authored by USDOT or funded partners. As a repository, ROSA P retains documents in their original published format to ensure public access to scientific information.

i

Computational Simulation of Large Droplet Icing

1996-01-01
By Wright, William B. ; Potapczuk, Mark G.

[PDF-634.07 KB]

English

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Creators:

Wright, William B. ; Potapczuk, Mark G.

Wright, William B. ; Potapczuk, Mark G. Less -
Subject/TRT Terms:

[+]

Aerodynamics Airfoils Analysis Droplet Trajectories Ice Accretion Icing Icing Conditions Large Droplet Icing LEWICE Mathematical Prediction Meteorological Phenomena NASA Lewis Research Center Performance Simulation Splashing Testing Wind Tunnels
DOI:

https://doi.org/10.21949/1403450
Resource Type:

Research Paper
NTL Classification:

NTL-AVIATION-Aviation Safety/Airworthiness
Abstract:

Certification for flight into known icing remains one of the more challenging goals for aircraft manufacturers. This activity has been further complicated by the current interest in large droplet icing. Due to the lack of data available on the meteorology of this phenomena, there is currently an incomplete picture of the nature of the condition and even less information on its impact on aerodynamic performance. This paper describes current simulation tools available at NASA Lewis Research Center, their capabilities, and future development goals with respect to large droplet icing simulation.
Format:

PDF
Collection(s):

US Transportation Collection
Main Document Checksum:

[+]

urn:sha256:072c207f82d7871183ab072e5a24675c7e32ce9d90b58c826379a183a7ce2dbf
Download URL:

https://rosap.ntl.bts.gov/view/dot/12878/dot_12878_DS1.pdf
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Computational Simulation of Large Droplet Icing

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