A Computational Investigation of Icing Effects on an S-Duct Inlet
نویسندگان
چکیده
منابع مشابه
A Computational Investigation of Icing effects on an S-Duct Inlet
The effects of a typical glaze ice accretion shape on the performance of the M2129 S-duct inlet are computationally investigated for a range of flight Mach numbers. A Reynolds-Averaged Navier-Stokes (RANS) code with k-o> turbulence model is used to simulate the compressible viscous flow in the S-duct inlet. The glaze ice accretion on the cowl lip is modeled on a steady-state basis f rom N A S A...
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ژورنال
عنوان ژورنال: International Journal of Turbo and Jet Engines
سال: 2010
ISSN: 2191-0332,0334-0082
DOI: 10.1515/tjj.2010.27.3-4.277