Combustion-Powered Actuation for Dynamic-Stall Suppression: High-Mach Simulations and Low-Mach Experiments-Reference-Cited by-同舟云学术

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Combustion-Powered Actuation for Dynamic-Stall Suppression: High-Mach Simulations and Low-Mach Experiments

Published:2015-08 Issue:8 Volume:53 Page:2151-2163
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Matalanis Claude G.,Min Byung-Young,Bowles Patrick O.,Jee Solkeun,Wake Brian E.,Crittenden Thomas M.,Woo George,Glezer Ari

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053641

Reference32 articles.

1. Miniature Trailing-Edge Effectors for Rotorcraft Performance Enhancement

2. Passive Control of Compressible Dynamic Stall

3. Dynamic Stall Control Using Deployable Leading-Edge Vortex Generators

4. Closed-loop Dynamic Stall Control Using a Plasma Actuator

5. High Mach Number Leading-Edge Flow Separation Control Using AC DBD Plasma Actuators

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1. Numerical Simulation of the Transient Flow around the Combined Morphing Leading-Edge and Trailing-Edge Airfoil;Biomimetics;2024-02-12

2. Numerical Study on Combustion-Driven Jet Actuation for Aerodynamic Control of Airfoil Flows;Energies;2023-12-11

3. Numerical investigation on high-speed jet actuation for transient control of flow separation;Aerospace Science and Technology;2023-04

4. Review of rotating wing dynamic stall: Experiments and flow control;Progress in Aerospace Sciences;2023-02

5. Numerical investigation of impulsively generated high-speed jet for dynamic stall suppression;Computers & Fluids;2023-01

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