Investigation of a method for the measurement of subsonic oscillatory aerodynamic influence coefficients,

"ASTIA document no. AD-142201."

Investigation of lateral stability at stall.

"Aeronautical Research Laboratory. Contract no. AF 33(038)-10480, RDO no. 472-106."

Stability of the boundary layer;

Reproduced from typewritten copy.

Development of a continuous flow electromagnetic alternating current traveling wave accelerator for high-density, hypervelocity wind tunnel applications,

Mode of access: Internet.

Vector polar method for shock interactions with area disturbances /

"AFOSR TN 59-701. Contract no. AF49(638)-166. I. E. R. project no. 96895."

Pressure gradient effects on supersonic boundary layer turbulence : final report /

"Carried out by the Fluid Mechanics Section of the Aeronutronic Division of the Ford Aerospace & Communications Corporation."

Boundary layer and wake modifications to compressor design systems : the effect of blade-to-blade flow variations on the mean flow field of a transonic rotor : final report, 01 September 1976-31 August 1978 /

"AFAPL-TR-79-2010."

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.

Drag due to lift of a not-so-slender configuration; application of theory.

"Contract no. AF 33(616)-2933."

Reduction of drag due to lift at supersonic speeds

"Aeronautical Research Laboratory, Contract no. AF 33(616)-2170, Project no. 1366."

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."

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

Mode of access: Internet.

Étude sur l'aviation,

Mode of access: Internet.

Linearized theory of conical supersonic flow with application to triangular wings /

Loose-leaf.

Flight without formula : simple discussions on the mechanics of the aeroplane /

Mode of access: Internet.