NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

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

Back to Results
Altitude Scaling of Thermal Ice Protection Systems in Running Wet OperationA study into the effects of altitude on an aircraft thermal Ice Protection System (IPS) performance has been conducted by the National Research Council Canada (NRC) in collaboration with the NASA Glenn Icing Branch. The study included tests of an airfoil model, with a heated-air IPS, installed in the NRCs Altitude Icing Wind Tunnel (AIWT) at altitude and ground level conditions.
Document ID
20180000400
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Orchard, D. M. (National Research Council of Canada Ottawa, Ontario, Canada)
Addy, H. E. (NASA Glenn Research Center Cleveland, OH, United States)
Wright, W. B. (Vantage Partners, LLC Cleveland, OH, United States)
Tsao, J. (Ohio Aerospace Inst. Cleveland, OH, United States)
Date Acquired
January 16, 2018
Publication Date
June 5, 2017
Subject Category
Aeronautics (General)
Report/Patent Number
GRC-E-DAA-TN42559
Report Number: GRC-E-DAA-TN42559
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics (AIAA) Aviation Aviation Technology, Integration, and Operations Conference
Location: Denver, CO
Country: United States
Start Date: June 5, 2017
End Date: June 9, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 081876.02.03.08.02.02
CONTRACT_GRANT: NNC12BA01B
CONTRACT_GRANT: NNC13BA10B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Running wet mode
Altitude scaling
Thermal ice protection system
upwind schemes
convention equation

Related Records

There are no records associated with this record.
No Preview Available