LEADER 02805oam  2200841   450 
001 9910709712803321
005 20180828111904.0
035   $a(CKB)5470000002473122
035   $a(OCoLC)761308948
035   $a(OCoLC)995470000002473122
035   $a(EXLCZ)995470000002473122
100   $a20111115j198605    ua             0
101 0 $aeng
135   $aurun||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aR4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel /$fRenaldo V. Jenkins
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dMay 1986.
215   $a1 online resource (111 pages) $cillustrations
225 1 $aNASA/TP ;$v2565
300   $aPrepared at Langley Research Center.
300   $a"May 1986."
320   $aIncludes bibliographical references (pages 9-10).
606   $aAirfoils$2nasat
606   $aReynolds number$2nasat
606   $aTransonic wind tunnels$2nasat
606   $aMach number$2nasat
606   $aBoundary layers$2nasat
606   $aAerofoils$xTesting$vStatistics
606   $aReynolds number
606   $aTransonic wind tunnels
606   $aWall pressure (Aerodynamics)
606   $aBoundary layer
606   $aAerofoils$xTesting$2fast
606   $aBoundary layer$2fast
606   $aReynolds number$2fast
606   $aTransonic wind tunnels$2fast
606   $aWall pressure (Aerodynamics)$2fast
608   $aStatistics.$2fast
608   $aStatistics.$2lcgft
615  7$aAirfoils.
615  7$aReynolds number.
615  7$aTransonic wind tunnels.
615  7$aMach number.
615  7$aBoundary layers.
615  0$aAerofoils$xTesting
615  0$aReynolds number.
615  0$aTransonic wind tunnels.
615  0$aWall pressure (Aerodynamics)
615  0$aBoundary layer.
615  7$aAerofoils$xTesting.
615  7$aBoundary layer.
615  7$aReynolds number.
615  7$aTransonic wind tunnels.
615  7$aWall pressure (Aerodynamics)
700   $aJenkins$b Renaldo V.$01409222
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
801  2$bMERUC
801  2$bGPO
906   $aBOOK
912   $a9910709712803321
996   $aR4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel$93495076
997   $aUNINA