Ultra Low Reynolds Number Airfoil Testing Facility

Author:

Kerho Michael1

Affiliation:

1. Rolling Hills Research Corporation

Publisher

American Institute of Aeronautics and Astronautics

Reference4 articles.

1. Erm, L. "An Investigation into the Feasibility of Measuring Flow-Induced Pressures on the Surface of a Model in theAMRLWater Tunnel,"DSTO-TN-0323,Nov.2000.

2. Sinclair, A. R. and Robbins, A. W. "A Method of the Determination of the Time Lag in Pressure Measuring SystemsIncorporating Capillaries,"NACATN2793,Sept.1952.

3. Schlichting,H.,Boundary-LayerTheory,7thEd., McGraw-HillPublishing,NewYork,1987,pp.758-764.

4. Experimental Investigation of the Wake-Survey Method for a Bluff Body with a Highly Turbulent Wake

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