1983-07-11

Aircraft De-icing Performance Analysis by an Adapted Temperature Field Analyser Program 831141

An evaluation of a special thermal mathematical model for anti- or de-icing purposes on airfoils and air inlets of air-crafts is described. The model using finite elements includes heat transfer by conduction, high speed convection for laminar or turbulent air flow, evaporation and mass transport.
The thermal mathematical model enables us to vary flight weather conditions, contour geometries, de-icing system details and the flight design cases with the combined turbine engine performance datas. The new mathematical model delivers a detailed matrix of surface temperatures and the running wet back water. The model flexibility will be demonstrated.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 43% off list price.
Login to see discount.
Special Offer: With TechSelect, you decide what SAE Technical Papers you need, when you need them, and how much you want to pay.
X