Work

Dynamic Stall Alleviation Using a Deformable Leading Edge Concept-A Numerical Study

Year: 2003

Type: article

Source: Journal of Aircraft

DOI: 10.2514/2.3060

Authors: Mehmet Sahin, Lakshmi N. Sankar, M. S. Chandrasekhara, Chee Tung

Institutions: Georgia Institute of Technology, Naval Postgraduate School, Ames Research Center

Language: English

Topic: Aeroelasticity and Vibration Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W2153602138

FWCI: 1.791

Cites: 14

Cited by: 37

Related to: 10