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Computational simulation of ice accretion and shedding trajectory of a rotorcraft in forward flight with strong rotor wakes

  • Published:2021-12 Issue: Volume:119 Page:107140
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Sengupta Bidesh,Raj L. PrinceORCID,Cho M.Y.,Son Chankyu,Yoon TaekeunORCID,Yee Kwanjung,Myong R.S.ORCID

Funder

National Research Foundation of Korea

Ministry of Science, ICT and Future Planning

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference93 articles.

1. Technically Advanced Aircraft-Safety and Training,2005

2. Subsonic aircraft safety icing study;Jones,2008

3. Interplay of unsteady aerodynamics and flight dynamics of transport aircraft in icing conditions;Ignatyev;Aerosp. Sci. Technol.,2020

4. New 3-D ice accretion method of hovering rotor including effects of centrifugal force;Zhao;Aerosp. Sci. Technol.,2016

5. Aircraft icing: an ongoing threat to aviation safety;Cao;Aerosp. Sci. Technol.,2018

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