Abstract
Discussions and sample results are presented for an in-flight wing ice accretion detector based on newly developed ultrasonic guided wave sensors and measurements. Detection over a fairly large area can be accomplished with these sensors. Physical principles, hardware, and computational methods are outlined along with a description of two flight demonstration programs. Excellent results are obtained, pointing to the potential for immediate field use of this new ice detection technology.
Original language | English (US) |
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DOIs | |
State | Published - Dec 1 2001 |
Event | SAE Advances in Aviation Safety Conference - 2001 Aerospace Congress - Seattle, WA, United States Duration: Sep 10 2001 → Sep 14 2001 |
Other
Other | SAE Advances in Aviation Safety Conference - 2001 Aerospace Congress |
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Country/Territory | United States |
City | Seattle, WA |
Period | 9/10/01 → 9/14/01 |
All Science Journal Classification (ASJC) codes
- Automotive Engineering
- Safety, Risk, Reliability and Quality
- Pollution
- Industrial and Manufacturing Engineering