Predicting Rotor Heat Transfer Using the Viscous Blade Element Momentum Theory and Unsteady Vortex Lattice Method

Calculating the unsteady convective heat transfer on helicopter blades is the first step in the prediction of ice accretion and the design of ice-protection systems. Simulations using Computational Fluid Dynamics (CFD) successfully model the complex aerodynamics of rotors as well as the heat transfe...

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Hlavní autoři:	Abdallah Samad, Gitsuzo B. S. Tagawa, François Morency, Christophe Volat
Médium:	Artigo
Jazyk:	Inglês
Vydáno:	MDPI AG 2020-07-01
Edice:	Aerospace
Témata:	unsteady vortex lattice method blade element momentum theory convective heat transfer icing/de-icing rotorcraft
On-line přístup:	https://www.mdpi.com/2226-4310/7/7/90
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