Static tests on prestresed concrete beams using 7/16 in. strands.

Mode of access: Internet.

A theory for the effect of mean stress on fatigue of metals under combined torsion and axial load or bending.

"Department of Army Project no. 5B99-01-004, Ordnance R and D Project no. TB2-0001, Office of Ordnance Research Project no. 1348, Contract no. DA-19-020-ORD-3250."

Modern installation for testing of large assemblies under static and fatigue loading. Description of installation at Fritz Engineering laboratory, Lehigh University, Bethlehem, Pennsylvania,

"Not for publication."

NONSAP : a structural analysis program for static and dynamic response of nonlinear systems /

Photocopy of original: Berkeley : Structural Engineering Laboratory, University of California, 1974.

Axial tension and bending interaction curves for members loaded inelastically,

Mode of access: Internet.

Round-robin pretest analyses of a 1:6-scale reinforced concrete containment model subject to static internal pressurization /

"SAND87-0891, R1 and RD."

A bending magnet with nonsaturating shimming /

"AEC Contract AT(04-3)-400."

Thermal effects on static aeroelastic stability and control.

v. 1. Methods of predicting structural temperatures due to aerodynamic heating, by A. H. Blessing.--v. 2. Aerodynamics, by J. R Batt.--v. 3. Experimental and analytical methods for the determination of thermally-affected wing deflectional behavior, by R. H. Gallagher.--v. 3. sup. Description and results of tests conducted to determine the thermally affected behavior of corrugated multiweb wing structures, by J. F. Quinn.

Supersonic aeroelastic effects on static stability and control. Flight Control Laboratory. Contract nos. AF33 (616)-3577 and AF33(616)-6067. ARDC Project no. 8219. Task no. 82158.

pt. 3. Aeroelastic interaction, by V. W. Donato.

Particle orbits in the static sheet pinch /

"April 1963."

Investigations on the basic theory of static and dynamic pressure phenomena in grain under conditions of storage

Cover title.

Investigation of helicopter rotor blade flutter and flapwise bending response in hovering

"Propulsion Laboratory, Contract no. AF33(616)-5210, Project no. 3137, Task no. 33113."

Automatic control of static electricity for Army helicopters; phase I report.

At head of title: Project 9R38-01-107-30. Contract DA 44-177-TC-652.

Automatic control of static electricity for army helicopters, October 1962.

"Task 9R38-01-017-30. Contract DA 44-177-TC-652."

Elements of static electricity with full description of the Holtz and Töpler machines and their mode of operating.

Mode of access: Internet.