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Lift improvements using duty-cycled plasma actuation at low Reynolds numbers

  • Published:2018-01 Issue: Volume:72 Page:123-133
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Meng XuanshiORCID,Hu HaiyangORCID,Yan Xu,Liu Feng,Luo ShijunORCID

Funder

National Natural Science Foundation of China

National Key Laboratory Research Foundation of China

111 Project

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference39 articles.

1. Low-Speed Wind Tunnel Test Results of the Canard Rotor/Wing Concept;Bass,1993

2. Sizing methodology for reaction-driven, stopped-rotor vertical takeoff and landing concepts;Crossley;J. Aircr.,1995

3. The Canard Rotor Wing (CRW) Aircraft – A New Way to Fly;Mitchell,1993

4. Fixed-Wing Performance Predictions of the Canard Rotor/Wing Conception Based on Wind Tunnel Test Results;Bass,1995

5. Summary of Low-Speed Airfoil Data, vol. 1;Selig,1995

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