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210210s1965 ohua bt f000 0 eng d |
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‡a(MiU)99187539718106381
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‡asdr-miu.99187539718106381
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‡aTRAAL
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‡aMAIN
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‡aD 301.45/26-3:63-449 Supplement 1
|
100 |
1 |
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‡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 |
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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 |
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⊔ |
‡av, 16 pages :
‡billustrations ;
‡c28 cm.
|
336 |
⊔ |
⊔ |
‡atext
‡btxt
‡2rdacontent
|
337 |
⊔ |
⊔ |
‡aunmediated
‡bn
‡2rdamedia
|
338 |
⊔ |
⊔ |
‡avolume
‡bnc
‡2rdacarrier
|
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0 |
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‡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.
|
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⊔ |
‡aMode of access: Internet.
|
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‡aVibration
‡xTesting.
|
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0 |
‡aMach number.
|
650 |
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‡aFlutter (Aerodynamics)
|
710 |
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‡aAir Force Flight Dynamics Laboratory (U.S.),
‡esponsor.
|
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⊔ |
‡aUnited States.
‡bAir Force.
‡bSystems Command.
‡bAeronautical Systems Division,
‡eissuing body.
|
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⊔ |
‡aBoeing Company,
‡esponsor.
|
730 |
0 |
⊔ |
‡aTechnical Report Archive & Image Library (TRAIL)
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‡a39015095317734
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