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The B-70'S New Structural Design Concepts for Mach 3 Temperatures Los Angeles Div., North American Aviation, Incorporated

SAE Technical Papers (1906-current) Available online

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Format:
Other
Author/Creator:
Clay, Eugene O., author.
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1962
Summary:
The B-70 is becoming a reality through an intensive design and fabrication development of a heat resistant, fuel insulating, primary structure, which permits long range cruise at Mach 3. The novel design features machine fusion welding for joining brazed, heat treated steel honeycomb-panels into a homogeneous, compression resistant structure, with local stresses and shear flow based upon minimum strain energy. With a background of continuing metallurgical research and development of fabrication techniques throughout its design and construction, the first stainless steel XB-70 is being readied for flight by year's end
Notes:
Vendor supplied data
Publisher Number:
620374
Access Restriction:
Restricted for use by site license

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