A mechanism for ice roughness formation on an airfoil leading edge, contributing to glaze ice accretion-Reference-Cited by-同舟云学术

A mechanism for ice roughness formation on an airfoil leading edge, contributing to glaze ice accretion

Published:1998-01-12 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Tsao J.¹,Rothmayer A.¹

Affiliation:

1. Iowa State Univ., Ames

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-485

Reference29 articles.

1. I.Lozowski,E.P.andOleskiw,M.M."Computer Modeling of Time-Dependent Rime Icing in the Atmosphere," CRREL Report 83-2,USAF, Jan. 1983.

2. Ruff, G.A.andBerkowitz,B.M. "UserManual fortheNASALewisIceAccretionPredictionCode (LEWICE),"NASA CR-185129, May. 1990.

3. Cansdale, J. T. and Gent, R. W. "IceAccretion on Airfoils in Two-Dimensional Compressible Flow - ATheoretical Model," Royal Aircraft Establishment Technical Report 82128, 1983.

4. Macarthur,C.D."NumericalSimulationofAirfoil Ice Accretion,"AIAA-83-0112,Jan. 1983.

5. Equilibrium Temperature of an Unheated Icing Surface as a Function of Air Speed

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