DIVISION OF ENGINEERING : SONIC BOOM EFFECTS ON STRUCTURES—A SIMPLIFIED APPROACH*
1968; Wiley; Volume: 30; Issue: 3 Series II Linguagem: Inglês
10.1111/j.2164-0947.1968.tb02482.x
ISSN2164-0947
AutoresD. Cheng, Jacques E. Benveniste,
Tópico(s)Vehicle Noise and Vibration Control
ResumoTransactions of the New York Academy of SciencesVolume 30, Issue 3 Series II p. 457-478 DIVISION OF ENGINEERING: SONIC BOOM EFFECTS ON STRUCTURES—A SIMPLIFIED APPROACH* David H. Cheng, David H. Cheng Department of Civil Engineering The City College of the City University of New York New York, N. Y.Search for more papers by this authorJacques E. Benveniste, Jacques E. Benveniste Department of Civil Engineering The City College of the City University of New York New York, N. Y.Search for more papers by this author David H. Cheng, David H. Cheng Department of Civil Engineering The City College of the City University of New York New York, N. Y.Search for more papers by this authorJacques E. Benveniste, Jacques E. Benveniste Department of Civil Engineering The City College of the City University of New York New York, N. Y.Search for more papers by this author First published: January 1968 https://doi.org/10.1111/j.2164-0947.1968.tb02482.xCitations: 7 † This paper, illustrated with slides, was presented at a meeting of the Division on December 13, 1967. AboutPDF ToolsRequest permissionExport citationAdd to favoritesTrack citation ShareShare Give accessShare full text accessShare full-text accessPlease review our Terms and Conditions of Use and check box below to share full-text version of article.I have read and accept the Wiley Online Library Terms and Conditions of UseShareable LinkUse the link below to share a full-text version of this article with your friends and colleagues. Learn more.Copy URL Share a linkShare onEmailFacebookTwitterLinkedInRedditWechat REFERENCES 1 WHITHAM, G. B. 1952. The flow pattern of a supersonic projectile. Comm. Pure and Appl. Math. 5: 301. 2 CARLSON, H. W., R. J. MACK & O. A. MORRIS. 1965. Sonic-boom pressure-field estimation techniques. Proc. Sonic Boom Symp., Acoust. Soc. Am. Nov.: 10. 3 MAGLIERI, D. J. 1965. Some effects of airplane operations and the atmosphere on sonic boom signatures. Proc. Sonic Boom Symp., Acoust. Soc. Am. Nov.: 36. 4 KANE, E. J. 1965. Some effects of the nonuniform atmosphere on the propagation of sonic booms. Proc. Sonic Boom Symposium, Acoust. Soc. Am. Nov.: 26. 5 KELLER, J. B. & A. BLANK. 1951. Diffraction and reflection of pulses by wedges and corners. Comm. Pure and Appl. Math. Ser. 4, No. 1. 6 HUBBARD, H. H., D. J. MAGLIERI, V. HUCKEL & D. A. HILTON. 1964. Ground measurements of sonic-boom pressures for the altitude range of 10,000 to 75,000 feet. NASA TR R-198. 7 HILTON, D. A., V. HUCKEL, R. STEINER & D. J. MAGLIERI. 1964. Sonic boom exposure during FAA community-response studies over a 6-month period in the Oklahoma City area. NASA TN D-2539. 8 CHENG, D. H. 1964. Some dynamic effects of sonic booms on building structural elements. LWP-25, NASA Langley Research Center. 9 CHENG, D. H. 1965. Dynamic response of structural elements to traveling N-shaped pressure waves. LWP-147, NASA Langley Research Center. 10 CHENG, D. H. & J. E. BENVENISTE. 1966. Transient response of structural elements to traveling pressure waves of arbitrary shape. Int. J. Mech. Sci. 8: 607–618. 11 JOHNSON, C. L. 1956. Analog Computer Techniques. McGraw-Hill Book Co., New York, N. Y.. Citing Literature Volume30, Issue3 Series IIJanuary 1968Pages 457-478 ReferencesRelatedInformation
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