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William E. Frazier
Researcher at Naval Air Systems Command
Publications - 20
Citations - 4230
William E. Frazier is an academic researcher from Naval Air Systems Command. The author has contributed to research in topics: Microstructure & Recrystallization (geology). The author has an hindex of 7, co-authored 13 publications receiving 3103 citations.
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Journal ArticleDOI
Metal Additive Manufacturing: A Review
TL;DR: The state-of-the-art of additive manufacturing (AM) can be classified into three categories: direct digital manufacturing, free-form fabrication, or 3D printing as discussed by the authors.
Journal ArticleDOI
The effect of thermal exposure on the mechanical properties of 2099-T6 die forgings, 2099-T83 extrusions, 7075-T7651 plate, 7085-T7452 die forgings, 7085-T7651 plate, and 2397-T87 plate aluminum alloys
J. Jabra,M. Romios,J. Lai,E.W. Lee,M. Setiawan,E. W. Lee,J. Witters,N. Abourialy,J. Ogren,R. Clark,T. Oppenheim,William E. Frazier,Omar S. Es-Said +12 more
TL;DR: In this article, the effect of thermal exposure on the mechanical properties and electrical conductivity of aluminum alloys was evaluated at temperatures ranging from 180 °C (350 °F) to 230°C (450 °F).
Journal ArticleDOI
The effect of thermal exposure on the electrical conductivity and static mechanical behavior of several age hardenable aluminum alloys
E. W. Lee,T. Oppenheim,K. Robinson,B. Aridkahari,N. Neylan,D. Gebreyesus,Martin Richardson,M. Arzate,C. Bove,Maria Emil Iskandar,C. Sanchez,E. Toss,I. Martinez,D. Arenas,J. Ogren,J. McLennan,R. Clark,William E. Frazier,Omar S. Es-Said +18 more
TL;DR: In this paper, the effects of heat damage on aluminum alloys were simulated and the correlations existing between the static mechanical and electrical conductivity properties were determined. And the results indicated that at the temperatures below 260 °C (500 °F) all five alloys showed clear correlations between the mechanical and physical properties.
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Qualifying of metallic materials and structures for aerospace applications
TL;DR: The U.S. Navy's certification and qualification process for materials and structures is undertaken to ensure the flight safety and full mission capability of naval aviation weapon systems as mentioned in this paper, where validated engineering data and concepts provide the foundation for continued technological development and innovation.
Journal ArticleDOI
The effect of retrogression and reaging on the properties of the 7249 aluminum alloy
TL;DR: In this paper, the retrogression and reaging (RRA) heat-treatment process and recent developments in high-strength 7xxx series aluminum alloys are summarized in this article.