Chord-wise air load distribution : War Dept., Army Air Forces : Navy Dept., Bureau of Aeronautics : Dept. of Commerce, Civil Aeronautics ... /

Tables.

Wind tunnel tests of thin airfoils oscillating near stall.

"January 1969."

Investigation of feasibility of utilizing available heat resistant materials for hypersonic leading edge applications.

"Volumes I through VIII are unclassified while volume IX is classified secret."

Computed moisture interception on helicopter rotor blades,

"Contract no. AF 33(616)-2859."

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.