Experimental and theoretical panel flutter studies in the mach number range of 1.0 to 5.0 : supplement 1

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049 ‡aMAIN
086 0 ‡aD 301.45/26-3:63-449 Supplement 1
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 : ‡bsupplement 1 / ‡cE. H. Dowell.
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, ‡c1965.
300 ‡av, 16 pages : ‡billustrations ; ‡c28 cm.
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aASD-TDR ; ‡v63-449 Supplement 1
500 ‡a"Project No. 1370, Task No. 137003."
500 ‡a"August 1965."
504 ‡aIncludes bibliographical references (page 12).
536 ‡aPrepared at Massachusetts Institute of Technology, under the The Boeing Company, Seatlle, Washington, Contract No. ‡bAF 33(616)-8081.
538 ‡aMode of access: Internet.
650 0 ‡aVibration ‡xTesting.
650 0 ‡aMach number.
650 0 ‡aFlutter (Aerodynamics)
710 2 ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor.
710 1 ‡aUnited States. ‡bAir Force. ‡bSystems Command. ‡bAeronautical Systems Division, ‡eissuing body.
710 2 ‡aBoeing Company, ‡esponsor.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
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