All Stories

  1. Mechanisms for turbulent separation control using plasma actuator at Reynolds number of 1.6 × 106
  2. Sound Generation of Flexible Plunging Wings in Hover at Low Reynolds Numbers
  3. Scaling Bioinspired Mars Flight Vehicles for Hover
  4. A Study on Development of Airfoil Shape Toward Low Reynolds-Number Dependence of Aerodynamic Characteristics Under Low-Reynolds-Number-Flow Conditions
  5. Plasma-Actuator Burst-Mode Frequency Effects on Leading-Edge Flow-Separation Control at Reynolds Number 2.6×105
  6. Analytical Aerodynamic Model of Spanwise Flexible Flapping Wings in Forward Flight
  7. Effects of Altitude on the Flight Performance of Monarch Butterflies
  8. Control of Dynamically Stalled Flowfield around a Pitching Airfoil by DBD Plasma Actuator
  9. Significance of Computational Spanwise Domain Length on LES for the Flowfield with Large Vortex Structure
  10. Multifactorial Effects of Operating Conditions of Dielectric-Barrier-Discharge Plasma Actuator on Laminar-Separated-Flow Control
  11. Propulsion of a Plunging Flexible Airfoil using a Torsion Spring Model
  12. Design Exploration of a DBD Plasma Actuator for Massive Separation Control
  13. LES of Separated-flow Controlled by DBD Plasma Actuator around NACA 0015 over Reynolds Number Range of 10^4-10^6
  14. Computational and Experimental Analysis of a High-Performance Airfoil Under Low-Reynolds-Number Flow Condition
  15. Effective Mechanisms for Turbulent-separation Control by DBD Plasma Actuator around NACA0015 at Reynolds Number 1,600,000
  16. Forward propulsion of a rigid plunging airfoil
  17. LES on Turbulent Separated Flow around NACA0015 at Reynolds Number 1,600,000 toward Active Flow Control
  18. Effect of Burst Frequency and Reynolds Number on Flow Control Authority of DBD Plasma Actuator on NACA0012 Airfoil
  19. Effects of Burst Frequency and Momentum Coefficient of DBD Actuator on Control of Deep-stall Flow around NACA0015 at Rec=2.6x10^{5}
  20. RANS-based Multi-Scale Simulations of a Scramjet Combustor