Abstract

T E use of models to predict the full-scale behavior of a structure is gaining increasing favor in the field of aeronautics. This t rend to model investigation is due not only to the saving in expense, labor, and time involved, bu t also to a better understanding of model laws and to recent improvements in the ar t of properly representing the prototype structure. Some time ago a practical type of model girder was developed, which permitted the axial, bending, and torsional elastic characteristics to be varied independently, and, further, it incorporated a convenient and sensitive means for measuring the corresponding strains and stresses. As a par t of an investigation program of the Special Committee on Airships a complete airship model, using this type of model member in place of the corresponding prototype girder, was constructed and tested. The work was carried ou t with the financial assistance of the Navy Department. The test program was carefully chosen so t ha t the effects of local loads could be conveniently isolated from the effects of general loads and in this way much of the confusion tha t has occurred in many previous model and full-scale tests was eliminated. M a n y variations of the structure were investigated such as with and without side or bot tom gangway and with high and low initial tension in the shear wiring. Fig. 1 shows a par t of the complete model rigged for test, with radial loads being applied to springs between the model and external loading rings.

Full Text
Paper version not known

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.