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The DESIGN of SHEET for PRODUCTION METAL AIRCRAFT PARTS

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
MALLETT, FRANK M., author.
Conference Name:
SAE National Aeronautic Meeting
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1944
Summary:
THE problem of sheet metal production design is separated into two parts, the determining of working limits of elongation and compression in different types of sheet metal forming, and the application of these limits to the design for formability. This paper is concerned with the second part of the problem.An analytical method of approach is suggested and is illustrated by five examples.In the case of curved flanges, flanged holes, and beads, formulas are given by which the amount of elongation or compression called for by the design may be computed directly from the dimensions given by the design.A possibility for a refinement in the use of the formulas is indicated, and an experimental method for achieving this refinement is pointed out
Notes:
Vendor supplied data
Publisher Number:
440205
Access Restriction:
Restricted for use by site license

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