LEADER 02336nam  2200613Ia 450 
001 9910699704503321
005 20101215111000.0
035   $a(CKB)5470000002405906
035   $a(OCoLC)692700998
035   $a(EXLCZ)995470000002405906
100   $a20101215d1984      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExtended parametric representation of compressor fans and turbines$b[electronic resource] /$f[G. L. Converse, R. G. Griffin]
210  1$aCincinnati, Ohio :$cGeneral Electric Company, Aircraft Engine Business Group, Advanced Technology Programs Dept. ;$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$d[1984]
215   $a1 online resource (3 volumes) $cdigital, PDF files
225 1 $aNASA CR ;$v174645
225 1 $aNASA CR ;$v174646
225 1 $aNASA CR ;$v174647
300   $a"March 1984."
300   $aTitle from title screen (viewed Dec. 14, 2010).
300   $a"Final report."
300   $a"Contract NAS3-23055."
320   $aIncludes bibliographical references: volume 1 (page 53) ; volume 2 (pages 50-52); volume 3 (page 46).
327   $aVol. I CMGEN user's manual -- Vol. II PART user's manual -- Vol. III MODFAN user's manual.
606   $aCentrifugal compressors$2nasat
606   $aCompressor rotors$2nasat
606   $aDesign analysis$2nasat
606   $aFlow stability$2nasat
606   $aModels$2nasat
606   $aParameterization$2nasat
606   $aTurbines$2nasat
606   $aUser requirements$2nasat
615  7$aCentrifugal compressors.
615  7$aCompressor rotors.
615  7$aDesign analysis.
615  7$aFlow stability.
615  7$aModels.
615  7$aParameterization.
615  7$aTurbines.
615  7$aUser requirements.
700   $aConverse$b George L$01395275
701   $aGriffin$b R. G$01395276
712 02$aGeneral Electric Company.$bAircraft Engine Business Group.$bAdvanced Technology Programs Department.
712 02$aLewis Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910699704503321
996   $aExtended parametric representation of compressor fans and turbines$93453510
997   $aUNINA