Experimental and theoretical panel flutter studies in the mach number range of 1.0 to 5.0

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035 ‡a(OCoLC)1194594498
035 ‡a(GWLA)gwla on1194594498
040 ‡aTRAAL ‡beng ‡cTRAAL
049 ‡aMAIN
086 0 ‡aD301.45/26-3: 63-449
100 1 ‡aDowell, E. H., ‡eauthor.
245 1 0 ‡aExperimental and theoretical panel flutter studies in the mach number range of 1.0 to 5.0 / ‡cE. H. Dowell and H. M. Voss.
264 1 ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, ‡c1963.
300 ‡axvi, 177 pages : ‡billustrations, figures, tables ; ‡c28 cm.
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aASD technical documentary report ; ‡v64-449
500 ‡a"Stamped: AD346621 (from http://www.dtic.mil)."
500 ‡a"(Prepared under Contract No. AF 33(616)-8081 by The Boeing Company, Seatlle 24, Washington)."
500 ‡a"Project No. 1370, Task No. 137002."
500 ‡a"December 1963."
504 ‡aIncludes bibliographical references (pages 40-42).
533 ‡aPrint reproduction.
538 ‡aMode of access: Internet.
583 1 ‡awill digitize ‡c20200828 ‡zQueued for digitization August 28, 2020 ‡5miu ‡2pda
650 0 ‡aVibration ‡xTesting.
650 0 ‡aMach number.
650 0 ‡aFlutter (Aerodynamics)
700 1 ‡aVoss, H. M., ‡eauthor.
710 2 ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡eissuing agency.
710 2 ‡aBoeing Company, ‡esponsor.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015095304138
CID ‡a102857333
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