LEADER 01831oam  2200493I  450 
001 9910691728603321
005 20171222125331.0
035   $a(CKB)5470000002348110
035   $a(OCoLC)1016449503
035   $a(OCoLC)995470000002348110
035   $a(EXLCZ)995470000002348110
100   $a20171222j200105    ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMAVRIC flutter model transonic limit cycle oscillation test /$fJohn W. Edwards [and four others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMay 2001.
215   $a1 online resource (15 pages) $cillustrations
225 1 $aNASA/TM ;$v2001-210877
300   $a"May 2001."
300   $a"This paper was presented at the 42nd AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, April 16-19, 2001, Seattle, Washington, AIAA Paper No. 2001-1291."
320   $aIncludes bibliographical references (page 15).
517 3 $aModels for aeroelastic validation research involving computation flutter model transonic limit cycle oscillation test
606   $aTransonic flow$2nasat
606   $aFlutter$2nasat
606   $aWind tunnel models$2nasat
606   $aWing tips$2nasat
606   $aWind tunnel tests$2nasat
615  7$aTransonic flow.
615  7$aFlutter.
615  7$aWind tunnel models.
615  7$aWing tips.
615  7$aWind tunnel tests.
700   $aEdwards$b John W.$0684
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910691728603321
996   $aMAVRIC flutter model transonic limit cycle oscillation test$93521675
997   $aUNINA