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Simulation Model Development for Icing Effects Flight Training
Technical Paper
2002-01-1527
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
A high-fidelity simulation model for icing effects flight training was developed from wind tunnel data for the DeHavilland DHC-6 Twin Otter aircraft. First, a flight model of the un-iced airplane was developed and then modifications were generated to model the icing conditions. The models were validated against data records from the NASA Twin Otter Icing Research flight test program with only minimal refinements being required. The goals of this program were to demonstrate the effectiveness of such a simulator for training pilots to recognize and recover from icing situations and to establish a process for modeling icing effects to be used for future training devices.
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Citation
Barnhart, B., Dickes, E., Gingras, D., and Ratvasky, T., "Simulation Model Development for Icing Effects Flight Training," SAE Technical Paper 2002-01-1527, 2002, https://doi.org/10.4271/2002-01-1527.Also In
References
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