Publication Date:
2019-07-13
Description:
A 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.
Keywords:
Aeronautics (General)
Type:
GRC-E-DAA-TN42559
,
American Institute of Aeronautics and Astronautics (AIAA) Aviation Aviation Technology, Integration, and Operations Conference; Jun 05, 2017 - Jun 09, 2017; Denver, CO; United States
Format:
application/pdf
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