A feasibility study on the development of a pre-crack fatigue damage indicator

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086 0 ‡aD 301.45/26-2:61-719
088 ‡aAD 277210
088 ‡aASD TR 61-719
100 1 ‡aKossar, Jerome M., ‡eauthor.
245 1 2 ‡aA feasibility study on the development of a pre-crack fatigue damage indicator / ‡cJerome M. Kossar.
264 1 ‡aWright-Patterson Air Force Base, Ohio : ‡bFlight Accessories Laboratory, Aeronautical Systems Division, Air Force Systems Command, ‡c1962.
300 ‡avi, 65 pages : ‡billustrations, tables ; ‡c28 cm.
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aAeronautical Systems Division (U.S.). Technical Report ; ‡vASD TR 61-719
500 ‡aAD 277210. Cover stamp.
500 ‡a"April 1962."
504 ‡aIncludes bibliographical references (page 14).
520 ‡aThe feasibility of the developement of a compact, remote indicating fatigue damage indicator is investigated. The investigation concerns several approaches to the prediction of fatigue failure primarily in 7075-T6 aluminum structure; however, some developed indicators may prove applicable to other structural materials. Test data are included for each of the techniques investigated. One of the gages developed in this program shows excellent promise of fulfilling the requirements of a fatigue damage indicator and is considered feasible for further development.
536 ‡aResearch supported by the United States Air Force, Air Force Systems Command, and performed by Republic Aviation Corporation, Farmingdale, New York, under Contract No. ‡bAF 33(616)-7103.
538 ‡aMode of access: Internet.
650 7 ‡aMetals ‡xCracking. ‡2fast ‡0(OCoLC)fst01018075
650 7 ‡aFatigue ‡xMeasurement. ‡2fast ‡0(OCoLC)fst00921942
650 0 ‡aMetals ‡xCracking.
650 0 ‡aFatigue ‡xMeasurement.
710 1 ‡aUnited States. ‡bAir Force. ‡bSystems Command. ‡bAeronautical Systems Division, ‡eissuing body.
710 2 ‡aRepublic Aviation Corporation, ‡esponsor.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015095318120
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