LEADER 01826nam  2200493Ia 450 
001 9910699793503321
005 20110124160703.0
035   $a(CKB)5470000002405007
035   $a(OCoLC)698130129
035   $a(EXLCZ)995470000002405007
100   $a20110124d2010      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSpreadsheet calculations for jets in crossflow$b[electronic resource]$eopposed rows of inline and staggered holes and single and opposed rows with alternating hole sizes /$fJames D. Holdeman, James R. Clisset, Jeffrey P. Moder
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2010]
215   $a1 online resource (33 pages) $cillustrations
225 1 $aNASA/TM- ;$v2010-216100
300   $aTitle from title screen (viewed on Jan. 24, 2011).
300   $a"July 2010."
320   $aIncludes bibliographical references (pages 12-13).
517   $aSpreadsheet calculations for jets in crossflow 
606   $aCross flow$2nasat
606   $aHole geometry (mechanics)$2nasat
606   $aGas turbine engines$2nasat
606   $aCombustion chambers$2nasat
606   $aMathematical models$2nasat
615  7$aCross flow.
615  7$aHole geometry (mechanics)
615  7$aGas turbine engines.
615  7$aCombustion chambers.
615  7$aMathematical models.
700   $aHoldeman$b J. D$01384589
701   $aClisset$b James R$01395514
701   $aModer$b Jeffrey P$01395515
712 02$aNASA Glenn Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910699793503321
996   $aSpreadsheet calculations for jets in crossflow$93454161
997   $aUNINA