Experimental Study of an Unsteady Separating Boundary Layer
Author:
Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.430
Reference24 articles.
1. Computation of Unsteady Flowfield over a Hydrofoil, Including Boundary Layer and Wake
2. Computation of Unsteady Viscous Marine-Propulsor Blade Flows—Part 1: Validation and Analysis
3. Unsteady Kutta Condition of a Plunging Airfoil
4. The response of airfoils to periodic disturbances - The unsteady Kutta condition
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