Stress and strain distribution in the vicinity of interference fit fasteners

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086 0 ⊔ ‡aD 301.45/46-2:72-153
088 ⊔ ⊔ ‡aAD 0760570
088 ⊔ ⊔ ‡aAFFDL TR 72-153
100 1 ⊔ ‡aAllen, Merle, ‡eauthor.
245 1 0 ‡aStress and strain distribution in the vicinity of interference fit fasteners / ‡cMerle Allen, J.A. Ellis.
264 ⊔ 1 ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, ‡c1973.
300 ⊔ ⊔ ‡aviii, 573 pages : ‡billustrations, tables ; ‡c28 cm.
336 ⊔ ⊔ ‡atext ‡btxt ‡2rdacontent
337 ⊔ ⊔ ‡aunmediated ‡bn ‡2rdamedia
338 ⊔ ⊔ ‡avolume ‡bnc ‡2rdacarrier
490 0 ⊔ ‡aAir Force Flight Dynamics Laboratory (U.S.). Technical report ; ‡vAFFDL TR 72-153
500 ⊔ ⊔ ‡aAD0760570 (from http://www.dtic.mil).
500 ⊔ ⊔ ‡a"January 1973."
520 ⊔ ⊔ ‡aA body of detailed stress and strain distributions in the vicinity of interference fit fasteners has been analytically obtained and is presented. These data, obtained on simple installations, present trends which may be used by designers in determining how or whether to use interference fit fasteners. The analysis was performed with a finite element digital procedure which has the nonlinear constitutive behavior programmed and interrelates internal loading and deformations. Preparations for the analysis of thirty six conditions included analyzing a test article for which good correlations are shown.
536 ⊔ ⊔ ‡aResearch supported by the Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, and performed by General Dynamics, Convair Aerospace Division, Fort Worth Operation, Fort Worth, Texas, under contract no. ‡bF33615-73-C-3026.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 7 ‡aStrains and stresses. ‡2fast ‡0(OCoLC)fst01134288
650 ⊔ 7 ‡aPlates (Engineering) ‡2fast ‡0(OCoLC)fst01066785
650 ⊔ 7 ‡aFasteners. ‡2fast ‡0(OCoLC)fst00921702
650 ⊔ 7 ‡aElastic plates and shells. ‡2fast ‡0(OCoLC)fst00904190
650 ⊔ 7 ‡aAluminum alloys. ‡2fast ‡0(OCoLC)fst00806309
650 ⊔ 0 ‡aFasteners.
650 ⊔ 0 ‡aStrains and stresses.
650 ⊔ 0 ‡aAluminum alloys.
650 ⊔ 0 ‡aElastic plates and shells.
650 ⊔ 0 ‡aPlates (Engineering)
700 1 ⊔ ‡aEllis, J. A., ‡eauthor.
710 1 ⊔ ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body.
710 2 ⊔ ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor.
710 2 ⊔ ‡aGeneral Dynamics Corporation. ‡bConvair Division, ‡esponsor.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
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DAT 1 ⊔ ‡a20231207140605.0 ‡b2024-07-02T17:31:57Z
DAT 2 ⊔ ‡a2024-07-02T17:30:02Z
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