Phase concerning relation of physical properties of spot welds to type of loads and service conditions experienced in aircraft has been given little attention; paper attempts to cover this phase with particular reference to primary structure of airplane; general review of factors that have limited use of spot welding in primary structure in past is included. (See also - v 44 n 3 Feb 1 1944 p 80, 84, 204, 207, 209-10, 214, n 5 Mar 1 p 121, 123, 125, 194, 196, 199)
Design of spot welded aluminum alloy aircraft structures
Aero Digest
Aero Digest ; 45 , n 1
1944
Aufsatz (Zeitschrift)
Englisch
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Fatigue Design of Welded Aluminum Structures
Online Contents | 1993
|Progress Report on Fatigue of Spot-welded Aluminum
NTRS | 1943
|Mechanical and corrosion tests of spot-welded aluminum alloys
Engineering Index Backfile | 1951
|Mechanical and corrosion tests of spot-welded aluminum alloys
TIBKAT | 1951
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