Theoretical analysis of the downstream influence of stagnation point mass transfer.

"Aeronautical Research Laboratory. Contract no. AF 33(616)-7064. Project no. 7064."

Flight text of an autopilot installation as a lateral gust alleviator in a PT-26 airplane.

"Aeronautical Research Laboratory. Contract No. AF 33(038)-10480, Task 70171, Project 1366."

Thermal buckling of circular cylindrical and conical thin-walled shells

"Aeronautical Research Laboratory. Contract AF 33(616)-3885, Project no. 7(8-1367), Task no. 70524."

Testing continuous computers.

"Aeronautical Research Laboratory, Contract No. AF33(616)-2797, Project 7060."

Combined effects of axial load, thermal stress, and creep in flat plates

"Aeronautical Research Laboratory. Contract AF33(616)-3617, Project 6-(8-1367) Task 70524."

Test of a model dynamic system synthesizer.

"Aeronautical Research Laboratory, Contract No. AF 33(616)-2797, Project 7060."

Investigation of lateral stability at stall.

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

Environmental pathways of selected chemicals in freshwater systems /

v. 1 issued October 1977 ; v. 2 issued May 1978.

Precipitation from solid solutions of metals. Abstract.

"Prepared for conference on "Phase transformations in solids" organized by National Research Council Committee on Solids, Cornell University, Aug. 23-27, 1948."

Oil Shale Symposium, Sampling, Analysis and Quality Assurance /

"Grant no. R806156."

An investigation of laminar heat transfer to slender cones in the hypersonic shock tunnel

"Contract no. AF-33(616)-6025. Project no. 7064. Task no. 70169. Aeronautical Research Laboratory, Air Force Research Division, Air Research and Development Command, United States Air Force, Wright-Patterson Air Force Base."

Helium injection into the boundary layer at an axisymmetric stagnation point

"Contract no. AF 33(616)-7661, Project no. 7064, Task no. 70169."

Reduction of drag due to lift at supersonic speeds

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

The structure of an electromagnetically driven shock,

"Prepared for the Air Force Ballistic Missile Division, Headquarters Air Research and Development Command, under Contract AF (04(647)-309, Thermonuclear Propulsion Research."

Design of the foam in place splint,

Mode of access: Internet.