LEADER 01643oam  2200553   450 
001 9910690034003321
005 20210324090553.0
035   $a(CKB)5470000002334924
035 9 $aocm31204277
035   $a(OCoLC)31204277
035   $a(EXLCZ)995470000002334924
100   $a19940930d1985      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBifurcation theory applied to aircraft motions /$fW.H. Hui, M. Tobak
210  1$aMoffett Field, California :$cNational Aeronautics and Space Administration, Ames Research Center,$d1985.
215   $a1 online resource (14 pages)
225 1 $aNASA technical memorandum ;$v86704
300   $a"March 1985."
320   $aIncludes bibliographical references (pages 10-11).
606   $aBifurcation theory
606   $aAerodynamics
606   $aAerodynamics$2fast
606   $aBifurcation theory$2fast
606   $aBranching (mathematics)$2nasat
606   $aAerodynamics$2nasat
615  0$aBifurcation theory.
615  0$aAerodynamics.
615  7$aAerodynamics.
615  7$aBifurcation theory.
615  7$aBranching (mathematics)
615  7$aAerodynamics.
700   $aHui$b W. H.$01382215
702   $aTobak$b Murray
712 02$aAmes Research Center,
801  0$bGPO
801  1$bGPO
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910690034003321
996   $aBifurcation theory applied to aircraft motions$93425433
997   $aUNINA