Tests of an area suction flap on an NACA 64A010 airfoil at high subsonic speeds /

Mode of access: Internet.

The effect of entrainment upon a jet-flapped airfoil.

"Submitted to the Office of Scientific Research of the Air Research and Development Command, United States Air Force, in partial fulfillment of contract number AF 18(600)-1523."

Theoretical and experimental studies of airfoil characteristics in nonuniform sheared flow.

At head of title: Task 1P125901A142. Contract DA 44-177-AMC-70 (T). USAAML technical report 65-17.

The influence of two-dimensional stream shear on airfoil maximum lift,

"Project 9R-38-01-000, Task 902. Contract DA 44-177-TC-439. U. S. Army Transportation Research Command, Transportation Corps, Fort Eustis, Virginia."

The two-dimensional effects of slipstream shear on airfoil characteristics

"Project no. 9-38-01-000, Task 902. Contract no. DA 44-177-TC-439."

The effects of axisymmetric shear on airfoil characteristics,

"Task 9R 38-11-009-03. Contract DA44-177-TC-439."

Tables of two-dimensional oscillating airfoil coefficients for rotary wings.

Mode of access: Internet.

Baseball Joe on the school nine; or, Pitching for the blue banner,

Mode of access: Internet.