Add to ORKGThe results of a research program to obtain design data on the strength of open-channel aluminum-alloy sections subjected to combined column and beam action. The results of the tests of about 70 specimens were graphed for stresses due to axial load and stresses due to bending loading as functions of length to radius of gyration of the specimens. From these graphs a design chart was derived that is suitable for ready use
The development of metal construction for aircraft has created a need for accurate and detailed info...
No rational column formula has yet been developed which gives results which are sufficiently precise...
The purpose of this investigation is to study the effect of repeated tensile stresses above the prop...
Column and plate compressive strengths of extruded 24S-T aluminum alloy were determined both within ...
The results of a research program to obtain design data on the strength of open-channel aluminum-all...
Extruded aluminum-alloy members of various cross sections are used in aircraft as compression member...
Report presents the results of a great number of tests made to determine the effect of service stres...
In the initial phase of a NACA program on fatigue research, axial-load tests on 24S-T3 and 75S-T6 al...
The general purpose in this study was to determine the stresses in a wooden member subjected to comb...
This report discusses the fundamental action of shear deformation of the flanges on the basis of sim...
Although a number of investigations of the bearing strength of aluminum alloys have been made, the p...
Laboratory tests were made to obtain information on the load-resisting properties of X76S-T aluminum...
Aerospace structures are optimally designed and analyzed to specifically-defined engineering paramet...
Values computed from an equation previously suggested by one of the authors for the critical stress ...
Design charts are developed for 24s-t aluminum-alloy flat compression panels with longitudinal z-sec...
The development of metal construction for aircraft has created a need for accurate and detailed info...
No rational column formula has yet been developed which gives results which are sufficiently precise...
The purpose of this investigation is to study the effect of repeated tensile stresses above the prop...
Column and plate compressive strengths of extruded 24S-T aluminum alloy were determined both within ...
The results of a research program to obtain design data on the strength of open-channel aluminum-all...
Extruded aluminum-alloy members of various cross sections are used in aircraft as compression member...
Report presents the results of a great number of tests made to determine the effect of service stres...
In the initial phase of a NACA program on fatigue research, axial-load tests on 24S-T3 and 75S-T6 al...
The general purpose in this study was to determine the stresses in a wooden member subjected to comb...
This report discusses the fundamental action of shear deformation of the flanges on the basis of sim...
Although a number of investigations of the bearing strength of aluminum alloys have been made, the p...
Laboratory tests were made to obtain information on the load-resisting properties of X76S-T aluminum...
Aerospace structures are optimally designed and analyzed to specifically-defined engineering paramet...
Values computed from an equation previously suggested by one of the authors for the critical stress ...
Design charts are developed for 24s-t aluminum-alloy flat compression panels with longitudinal z-sec...
The development of metal construction for aircraft has created a need for accurate and detailed info...
No rational column formula has yet been developed which gives results which are sufficiently precise...
The purpose of this investigation is to study the effect of repeated tensile stresses above the prop...