Altitude Scaling of Thermal Ice Protection Systems in Running Wet Operation-Reference-Cited by-同舟云学术

Altitude Scaling of Thermal Ice Protection Systems in Running Wet Operation

Published:2019-03 Issue:2 Volume:56 Page:607-620
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Orchard D. M.¹,Addy H. E.²,Wright W. B.³,Tsao J.²

Affiliation:

1. National Research Council Canada, Ottawa, Ontario K1A 0R6, Canada

2. NASA Glenn Research Center, Cleveland, Ohio 44135

3. Vantage Partners, LLC, NASA Glenn Research Center, Cleveland, Ohio 44135

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034892

Reference19 articles.

1. AddyH. E.OrchardD. M.WrightW. B.OleskiwM. “Altitude Effects on Thermal Ice Protection System Performance; a Study of an Alternative Approach,” NASA TM-219081, May 2016.

2. Characteristics of Runback Ice Accretions on Airfoils and their Aerodynamics Effects

3. WhalenE. A.BroerenA. P.BraggM. B. “Characteristics of Runback Ice Accretions and their Aerodynamic Effects,” Federal Aviation Administration TR DOT/FAA/AR-07/16, Washington, D.C. April 2007.

4. Icing Tunnel Experiments with a Hot Air Anti-Icing System

5. Aerodynamics of Scaled Runback Ice Accretions

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