Implicit LES of Noise Reduction for a Compressible Deep Cavity Using Pulsed Nanosecond Plasma Actuator

  • Z. L. ChenEmail author
  • B. Q. Zhang
  • S. Hickel
  • N. A. Adams
Conference paper
Part of the ERCOFTAC Series book series (ERCO, volume 20)


High-subsonic cavity flows have been intensively studied due to their practical importance in aeronautical applications, such as, weapon bays, measurement windows and wheel wells [1].


Shear Layer Sound Pressure Level Spanwise Direction Cavity Flow Plasma Actuator 
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Copyright information

© Springer International Publishing Switzerland 2015

Authors and Affiliations

  • Z. L. Chen
    • 1
    Email author
  • B. Q. Zhang
    • 1
  • S. Hickel
    • 2
  • N. A. Adams
    • 2
  1. 1.School of AeronauticsNorthwestern Polytechnical UniversityXi’anPeople’s Republic of China
  2. 2.Institute of Aerodynamics and Fluid MechanicsTechnische Universität MünchenMunichGermany

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