Effects of leading-edge ice accretion geometry on airfoil performance-Reference-Cited by-同舟云学术

Effects of leading-edge ice accretion geometry on airfoil performance

Published:1999-06-28 Issue: Volume: Page:
ISSN:
Container-title:17th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Kim Han¹,Bragg Michael¹

Affiliation:

1. Illinois, Univ., Urbana

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-3150

Reference23 articles.

1. 'Hoemer,S.F.andBorst,H. F. Fluid-DvnamicLift, HoemerFluidDynamics,Brick Town,N.J., 1975.

2. 'Weick, FredandE. Scudder,NathanF.,he Effect on Lift, Drag,andSpinningCharacteristicsof Sharp LeadingEdgesonAirplaneWings0022,NACA TN 447, February1933.

3. 4Ingehnan-Sundberg,M. andTnmov, O.K. "Wind TunnelInvestigationof theHazardousTail StallDue to Icing0022, ajoint reportfromtheSwedish-Soviet Working Groupfor Flight Safety,1979.

4. 'Ingelman-St&berg, M. andTrunov,O.K. "On the Problemof HorizontalTail StallDuetoIce0022, ajoint reportfrom theSwedish-SovietWorking Groupfor Flight Safety,1985.

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