A study of the parameters associated with employing laser speckle correlation fringes to measure in-plane strain

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088 ⊔ ⊔ ‡aAD 0744489
088 ⊔ ⊔ ‡aAFFDL TR 72-20
100 1 ⊔ ‡aAdams, Frank D.
245 1 2 ‡aA study of the parameters associated with employing laser speckle correlation fringes to measure in-plane strain / ‡cFrank D. Adams.
260 ⊔ ⊔ ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Air Force Systems Command, ‡c1972.
300 ⊔ ⊔ ‡avi, 19 p. : ‡bill. ; ‡c28 cm.
490 0 ⊔ ‡aTechnical report (Air Force Flight Dynamics Laboratory (U.S.)) ; ‡vAFFDL-TR-72-20
500 ⊔ ⊔ ‡a"This report is the result of an in-house effort conducted under Project 1467, 'Structural Analysis Methods,' Task 146702, 'Thermoelastic Structural Analysis Methods."-- P. ii.
500 ⊔ ⊔ ‡aDefense Technical Information Center accession number: AD0744489.
500 ⊔ ⊔ ‡a"March 1972."
500 ⊔ ⊔ ‡aCover title.
504 ⊔ ⊔ ‡aIncludes bibliographical references (p. 19).
520 3 ⊔ ‡a"Basic experimental parameters associated with using laser speckle correlation fringes to measure in-plane strain have been investigated. Equations and inequalities are derived which provide bounding numbers for many of the physical parameters. The feasibility of employing this technique for obtaining in-plane strain data in a microscopic region is shown. This suggests that it may be applicable for studying strain distributions in the vicinity of either a crack or an interference fit fastener." -- Abstract.
530 ⊔ ⊔ ‡aAlso available via the DTIC website: ‡uhttp://handle.dtic.mil/100.2/AD744489.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aHolographic interferometry.
650 ⊔ 0 ‡aStructural analysis (Engineering)
650 ⊔ 0 ‡aLaser speckle.
710 2 ⊔ ‡aAir Force Flight Dynamics Laboratory (U.S.)
CID ⊔ ⊔ ‡a011422340
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DAT 2 ⊔ ‡a2024-08-15T17:30:02Z
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