Experimental Investigations Of A Trailing Edge Noise Feedback Mechanism On A NACA 0012 Airfoil

·2013·DOI

Engineering and Technology

Aerospace Engineering

Aerodynamics and Flight Dynamics

Computational Methods in Aeroacoustics

Role in the Field

Neutralin Engineering and Technology

Neutralin Aerospace Engineering

Neutralin Aerodynamics and Flight Dynamics

Neutralin Computational Methods in Aeroacoustics

Abstract

Citations

64

Year

2013

PageRank

1.1 / 10

Relative influence (log-scaled)

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