Abstract
T TWO STUDIES HERE REPORTED are phases of a broad investigation of techniques of flutter analysis made for the Bureau of Aeronautics of the Navy Department [Contract Noa(s)-8790]. More complete accounts of the work, with full details of sample computations, are contained in the reports submitted to the Bureau. Companion reports cover applications of the Station Function method to the vibration and flutter analysis of a twin-engined aircraft and the development of methods of making and evaluating vibration tests on wings with and without concentrated masses at subcritical air speeds. All these reports may be obtained through the Bureau of Aeronautics. Contributions to the two studies covered by the present paper were made by G. Zartarian, S. M. Haley, G. Fotieo, H. J. Cunningham, P. T. Hsu, and E.'Moll0Christensen. Early survey work on the density variation scheme was done by J. Stevens, now with Chance Vought Aircraft; in some of the later work on the scheme, I. Spielberg, from Wright Field, took part. Appreciation is expressed to the Bureau of Aeronautics for its permission of the use of the material for this paper.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
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.