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Iced Aircraft Flight Data for Flight Simulator Validation
ISSN: 0148-7191, e-ISSN: 2688-3627
Published April 16, 2002 by SAE International in United States
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NASA is developing and validating technology to incorporate aircraft icing effects into a flight training device concept demonstrator. Flight simulation models of a DHC-6 Twin Otter were developed from wind tunnel data using a subscale, complete aircraft model with and without simulated ice, and from previously acquired flight data. The validation of the simulation models required additional aircraft response time histories of the airplane configured with simulated ice similar to the subscale model testing. Therefore, a flight test was conducted using the NASA Twin Otter Icing Research Aircraft.
Over 500 maneuvers of various types were conducted in this flight test. The validation data consisted of aircraft state parameters, pilot inputs, propulsion, weight, center of gravity, and moments of inertia with the airplane configured with different amounts of simulated ice. Emphasis was made to acquire data at wing stall and tailplane stall since these events are of primary interest to model accurately in the flight training device. Analyses of several datasets are described regarding wing and tailplane stall. Key findings from these analyses are that the simulated wing ice shapes significantly reduced the CL max, while the simulated tail ice caused elevator control force anomalies and tailplane stall when flaps were deflected 30⍛ or greater. This effectively reduced the safe operating margins between iced wing and iced tail stall as flap deflection and thrust were increased.
This flight test demonstrated that the critical aspects to be modeled in the icing effects flight training device include: iced wing and tail stall speeds, flap and thrust effects, control forces and control effectiveness.
|Technical Paper||Ultrasonic In-Flight Wing Ice Detection|
|Technical Paper||Smart Icing Systems for Aircraft Icing Safety|
|Aerospace Standard||Design Objectives For Handling Qualities Of Transport Aircraft|
CitationRatvasky, T., Blankenship, K., Rieke, W., and Brinker, D., "Iced Aircraft Flight Data for Flight Simulator Validation," SAE Technical Paper 2002-01-1528, 2002, https://doi.org/10.4271/2002-01-1528.
- Tailplane Icing, NASA Glenn, video tape, 1998. http://icebox.grc.nasa.gov/ext/education/video/video.html
- Icing for Regional and Corporate Pilots, NASA Glenn, video tape, 1999 http://icebox.grc.nasa.gov/ext/education/video/video.html
- In-Flight Icing, NASA Glenn, CD-ROM, 2000 http://icebox.grc.nasa.gov/ext/education/cbt/cbt.html
- Papadakis M., Gile-Laflin B., Youssef G., Ratvasky T., Aerodynamic Scaling Experiments with Simulated Ice Accretions, AIAA 2001-0833, January 2001
- Barnhart B., Dickes E., Gingras D., Ratvasky T., Simulation Model Development for Icing Effects Flight Training, SAE 2002-01-1527, April 2002
- Ratvasky T., Van Zante J., Sim A., NASA/FAA Tailplane Icing Program: Flight Test Report, NASA TP-2000-20908, March 2000
- Ranaudo R., Ratvasky T., Van Zante J., Flying Qualities Evaluation of a Commuter Aircraft With an Ice Contaminated Tailplane, NASA TM-2000-210356 SAE 2000-01-1676, September 2000
- Bihrle Applied Research Inc. http://www.bihrle.com/