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Experimental investigation of water impingement on single and multi-element airfoils

  • Published:2000-01-10 Issue: Volume: Page:
  • ISSN:
  • Container-title:38th Aerospace Sciences Meeting and Exhibit
  • language:
  • Short-container-title:

Author:

Papadakis Michael1,Hung Kuohsing1,Yeong Hsiung-Wei1,Bidwell Colin2,Breer Marlin3

Affiliation:

1. Wichita State Univ., KS

2. NASA, Glenn Research Center, Cleveland, OH

3. Boeing Commercial Airplane Group, Wichita, KS

Publisher

American Institute of Aeronautics and Astronautics

Reference170 articles.

1. provided in Table 3 and in Figs. 9-18. All tests were

2. aviation sections (t,Jc = 0.143 - 0.17) to thin

3. sections (t&c = 0.08 - 0.09) designed for high

4. the mid 1970's for general aviation aircraft (Ref.

5. was designed in the early 1980's for general

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1. Numerical Simulation of Supercooled Large Droplet Icing Phenomenon: A Review;Archives of Computational Methods in Engineering;2019-07-01

2. A numerical study of Supercooled Large Droplets’ impingement on airfoils;23rd AIAA Computational Fluid Dynamics Conference;2017-06-02

3. Investigation of water impingement on a multi-element high-lift airfoil by Lagrangian and Eulerian approach;Propulsion and Power Research;2015-09

4. Lagrangian Approach for Simulating Supercooled Large Droplets’ Impingement Effect;Journal of Aircraft;2015-03

5. Quasi-3D Multi-Step Ice Accretion Simulation;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09
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