Progress in Rotorcraft Icing Computational Tool Development

Richard E. Kreeger, Lakshmi Sankar, Robert Narducci, Robert Francis Kunz

Research output: Contribution to journalConference article

6 Scopus citations

Abstract

The formation of ice over lifting surfaces can affect aerodynamic performance. In the case of helicopters, this loss in lift and the increase in sectional drag forces will have a dramatic effect on vehicle performance. The ability to predict ice accumulation and the resulting degradation in rotor performance is essential to determine the limitations of rotorcraft in icing encounters. The consequences of underestimating performance degradation can be serious and so it is important to produce accurate predictions, particularly for severe icing conditions. The simulation of rotorcraft ice accretion is a challenging multidisciplinary problem that until recently has lagged in development over its counterparts in the fixed wing community. But now, several approaches for the robust coupling of a computational fluid dynamics code, a rotorcraft structural dynamics code and an ice accretion code have been demonstrated.

Original languageEnglish (US)
JournalSAE Technical Papers
Volume2015-June
Issue numberJune
DOIs
StatePublished - Jun 15 2015
EventSAE International Conference on Icing of Aircraft, Engines, and Structures, ICE 2015 - Prague, Czech Republic
Duration: Jun 22 2015Jun 25 2015

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All Science Journal Classification (ASJC) codes

  • Automotive Engineering
  • Safety, Risk, Reliability and Quality
  • Pollution
  • Industrial and Manufacturing Engineering

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