De-Icing Fluid Flow-Off from a Flat Plate in an Accelerating Airstream-Reference-Cited by-同舟云学术

De-Icing Fluid Flow-Off from a Flat Plate in an Accelerating Airstream

Published:2020-04 Issue:4 Volume:58 Page:1607-1619
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Koivisto P.¹,Honkanen T.²,Auvinen M.³,Hellsten A.³,Kahma K.³

Affiliation:

1. Aalto University, FI-00076 Aalto, Finland

2. Arteform Ltd., FI-02150 Espoo, Finland

3. Finnish Meteorological Institute, SF-00101 Helsinki, Finland

Funder

Liikenteen Turvallisuusvirasto Trafi

Federal Aviation Administration

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058706

Reference38 articles.

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2. HillE. G. “Aerodynamic AcceptanceTest forAircraft Ground Deicing/Anti-Icing Fluids,” Boeing Doc. D6-55573, BoeingCo., Seattle, WA, Oct. 1990.

3. RunyanL. J.ZiertenT. A.HillE. G.AddyH. E. “Lewis Icing Research Tunnel Test of the Aerodynamic Effects of Aircraft Ground Deicing/Anti-Icing Fluids,” NASA TP 3238, Aug. 1992.

4. Influence of Environmental Factors on Aircraft Performance;Hendrickson G. S.,1987

5. CarbonaroM. “Experimental Study of the Flow of a Film of Aircraft Deicing Fluid During a Simulated Take Off at Subfreezing Temperature,” von Karman Inst. for Fluid Dynamics CR1985-02, Brussels, May 1985.

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