Experimental Investigation of Supercooled Water Droplet Breakup near Leading Edge of Airfoil-Reference-Cited by-同舟云学术

Experimental Investigation of Supercooled Water Droplet Breakup near Leading Edge of Airfoil

Published:2018-09 Issue:5 Volume:55 Page:1970-1984
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Veras-Alba Belen,Palacios Jose,Vargas Mario,Ruggeri Charles,Bartkus Tadas P.¹

Affiliation:

1. Ohio Aerospace Institute, Cleveland, Ohio 44135

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034714

Reference11 articles.

1. TanJ.PapadakisM.SampathM. K. “Computational Study of Large Droplet Breakup in the Vicinity of an Airfoil,” Final Rept. DOT/FAA/AR-05/42, Witchita State Univ., Oct. 2005.

2. Rotating Arm-Based Experimental Study on Droplet Behavior in the Shoulder Region of an Aircraft Aerodynamic Surface

3. Rotating Rig Development for Droplet Deformation/Breakup and Impact Induced by Aerodynamic Surfaces

4. Mechanism of Water Droplet Breakup near the Leading Edge of an Airfoil

5. Effects of ice accretions on aircraft aerodynamics

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