Filament Wound Structural Model Studies for Deep Submergence Vehicles
1965; Wiley; Volume: 77; Issue: 2 Linguagem: Inglês
10.1111/j.1559-3584.1965.tb05358.x
ISSN1559-3584
AutoresNicholas D. Myers, Bruce K. Fink,
Tópico(s)Electromagnetic Launch and Propulsion Technology
ResumoNaval Engineers JournalVolume 77, Issue 2 p. 275-290 Filament Wound Structural Model Studies for Deep Submergence Vehicles N. MYERS, N. MYERS Norbert C. Myers, B.S., Aeronautical Engineering, Northrop Institute of Technology. Currently engaged in structural and materials research concerning reinforced plastics, particularly the filament-winding process. Past experience includes four years with Northrop Corporation, 9 years with the Zenith Plastics Division of Minnesota Mining & Manufacturing Company, and two years with the H. I. Thompson Fiber Glass Company. Mr. Myers is presently manager of the Structural Development Section.Search for more papers by this authorB. FINK, B. FINK Mr. Fink has served the aircraft and aerospace industry in the capacity of an engineering specialist for the past twenty-three years. He has participated extensively in programs covering the total spectrum in development of aircraft, both fixed and rotary wing, ground effect machines, fiber glass boats, plastic rocket motor cases and currently fiber reinforced plastic structures. Mr. Fink has had long and successful associations with Vehicle Research Corp., Aerojet General, Glasspar Boat, Fairchild Stratos, Norair and other organizations. Now he is employed as a Technical Specialist at H. I. Thompson Fiber Glass Co. He held a degree in Aeronautical Engineering from Pasadena City College and has studied at Universities of Southern California and California. He is a registered Professional Engineer of the State of California (NE 6962).Search for more papers by this author N. MYERS, N. MYERS Norbert C. Myers, B.S., Aeronautical Engineering, Northrop Institute of Technology. Currently engaged in structural and materials research concerning reinforced plastics, particularly the filament-winding process. Past experience includes four years with Northrop Corporation, 9 years with the Zenith Plastics Division of Minnesota Mining & Manufacturing Company, and two years with the H. I. Thompson Fiber Glass Company. Mr. Myers is presently manager of the Structural Development Section.Search for more papers by this authorB. FINK, B. FINK Mr. Fink has served the aircraft and aerospace industry in the capacity of an engineering specialist for the past twenty-three years. He has participated extensively in programs covering the total spectrum in development of aircraft, both fixed and rotary wing, ground effect machines, fiber glass boats, plastic rocket motor cases and currently fiber reinforced plastic structures. Mr. Fink has had long and successful associations with Vehicle Research Corp., Aerojet General, Glasspar Boat, Fairchild Stratos, Norair and other organizations. Now he is employed as a Technical Specialist at H. I. Thompson Fiber Glass Co. He held a degree in Aeronautical Engineering from Pasadena City College and has studied at Universities of Southern California and California. He is a registered Professional Engineer of the State of California (NE 6962).Search for more papers by this author First published: April 1965 https://doi.org/10.1111/j.1559-3584.1965.tb05358.xCitations: 9 AboutPDF ToolsExport 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 onFacebookTwitterLinked InRedditWechat Citing Literature Volume77, Issue2April 1965Pages 275-290 RelatedInformation
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