In this paper a cold soak fuel frost modeling for an aircraft wing tank is presented. Numerical prediction is compared with experimental data and a qualitative verification for the frost formation and melting is also shown. The numerical simulation showed good agreement with experimental observations. The model was used to define, through a Monte Carlo analysis, two different frost formations whose impact on aircraft handling was evaluated by flight tests using representative grits.
On-Ground Cold Soak Fuel Frost Modeling
Sae Technical Papers
International Conference on Icing of Aircraft, Engines, and Structures ; 2019
2019-06-10
Aufsatz (Konferenz)
Englisch
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