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Development and Utility of a Piloted Flight Simulator for Icing Effects Training
Author(s) -
Thomas Ratvasky,
Richard Ranaudo,
Billy Barnhart,
Edward Dickes,
David Gingras
Publication year - 2003
Publication title -
41st aerospace sciences meeting and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2003-22
Subject(s) - airframe , icing , flight simulator , cockpit , aeronautics , flight training , simulation , training (meteorology) , engineering , fidelity , aerospace engineering , computer science , marine engineering , meteorology , physics , electrical engineering
A piloted flight simulator called the Ice Contamination Effects Flight Training Device (ICEFTD), which uses low cost desktop components and a generic cockpit replication is being developed. The purpose of this device is to demonstrate the effectiveness of its use for training pilots to recognize and recover from aircraft handling anomalies that result from airframe ice formations. High-fidelity flight simulation models for various baseline (non-iced) and iced configurations were developed from wind tunnel tests of a subscale DeHavilland DHC-6 Twin Otter aircraft model. These simulation models were validated with flight test data from the NASA Twin Otter Icing Research Aircraft, which included the effects of ice on wing and tail stall characteristics. These simulation models are being implemented into an ICEFTD that will provide representative aircraft characteristics due to airframe icing. Scenario-based exercises are being constructed to give an operational-flavor to the simulation. Training pilots will learn to recognize iced aircraft characteristics from the baseline, and will practice and apply appropriate recovery procedures to a handling event.

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