Psychological stress as a theoretical concept.

"Project no. 7193."

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

"ASTIA document no. AD-142201."

The effect of metallurgical variables on the fatigue properties of AISI 4340 steel heat treated in the tensile strength range 260,000-310,000 psi

"Materials Laboratory. Contract no. AF 33(616)-3299, Project no. 7360."

Relationships between airman interests and career satisfaction.

"ASTIA document no. AD151 038."

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."

Literature survey of the corrosion of magnesium and magnesium alloys

"Materials Laboratory. Contract no. AF 33(616)-3032, Project no. 7351."

Microfilm aperture card system

"Conducted under ARDC Research and Development project 2079."

The mathematics of personnel utilization models,

Mode of access: Internet.

The development of oscillatory rolling-contact bearings for airframe applications in the temperature range 300 F to 600 F

"Aircraft Laboratory, ContractNo. AF 33(600)-34097, Project No. 1315."

Steady state undamped vibrations of a class of nonlinear discrete systems

"Materials Laboratory, Contract no. AF 33(616)-5449. Project no. 7360."

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."

Feasibility of a method for estimating short-term and long-term effects of policy decisions on the airman personnel,

"ASTIA document no. AD 217 079."

Damping of flexural vibrations by alternate visco-elastic and elastic layers

"Materials Laboratory, Contract no. AF 33(616)-5426, Project no. 7360."

A survey of dispersion strengthening of metals and alloys, [summary technical report,

Leaves 102-246 issued separeately as "Part II-Appendices."