Experimental investigation of the two-dimensional asymmetrical turbulent wake behind a blade

Author:

Ghazi M. A.1,Fathalah K. A.1,Rashed M. I.2,El-Taher R. M.1

Affiliation:

1. King Abdulaziz University, Jeddah, Saudi Arabia

2. Cairo University, Cairo, Egypt

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference12 articles.

1. 2Chan, Y.Y. "Small Cross-Flow in Three-Dimensional Laminar Boundary Layers with Suction or Injection," Aero Report LR-520, National Aeronautical Establishment, Ottawa, Canada, Feb. 1969.

2. 4Chan, Y.Y., Tang, F.C., and Wolfe, S.M. "Analysis of the Boundary Layer Development on the Side Walls of the NAE 2-D Test Facility," Laboratory Technical Report LTR-HA-34, National Aeronautical Establishment, Ottawa, Canada, Nov. 1978.

3. Development of modern airfoil sections for high subsonic cruise speeds

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