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Trajectory Simulation of Ice Shed From a Business Jet
Technical Paper
2003-01-3032
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
Trajectories of ice shed from two variants of a business jet were computed to show that a change in fuselage length did not increase the risk of ice ingestion by the engine. A droplet trajectory code modified for solid ice shapes, was used in the analysis. This method could help reduce icing flight tests when minor modifications are made to an aircraft.
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Citation
Chandrasekharan, R. and Hinson, M., "Trajectory Simulation of Ice Shed From a Business Jet," SAE Technical Paper 2003-01-3032, 2003, https://doi.org/10.4271/2003-01-3032.Also In
References
- Reehorst, A. L. “Study of Water Droplet Trajectories in the NASA Lewis Research Center Icing Research Tunnel (IRT)” NASA TM 107221 1996
- Hoerner, S. F. “Fluid Dynamic Drag” Hoerner Fluid Dynamics 1965