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001 9910717012003321
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100   $a20220106j199204    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model /$fAparajit J. Mahajan [and three others]
210  1$aWashington, D.C. :$cNASA,$dApril 1992.
215   $a1 online resource (approximately 14 pages) $cillustrations
225 1 $aNASA/TM ;$v105268
300   $a"April 1992."
320   $aIncludes bibliographical references (pages 6-7).
606   $aProp-fan technology$2nasat
606   $aFlutter$2nasat
606   $aCruise missiles$2nasat
615  7$aProp-fan technology.
615  7$aFlutter.
615  7$aCruise missiles.
700   $aMahajan$b Aparajit J$g(Aparajit Jagannath),$01419987
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
801  2$bGPO
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910717012003321
996   $aAeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model$93536332
997   $aUNINA