LEADER 01806oam  2200529   450 
001 9910704205203321
005 20160218114037.0
035   $a(CKB)5470000002439627
035   $a(OCoLC)755257955
035   $a(EXLCZ)995470000002439627
100   $a20111002j199610    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWing leading edge joint laminar flow tests /$fAaron Drake [and four others]
210   $aMoffett Field, California $cNational Aeronautics and Space Administration, Ames Research Center$dOctober 1996
215   $a1 online resource (33 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4762
300   $aTitle from title screen (viewed Feb. 18, 2016).
300   $a"October 1996."
300   $a"Performing organization: Ames Research Center, Moffett Field, CA"--Report documentation page.
320   $aIncludes bibliographical references (page 5).
606   $aF-104 aircraft$2nasat
606   $aLaminar flow airfoils$2nasat
606   $aFriction measurement$2nasat
606   $aSkin friction$2nasat
606   $aPressure distribution$2nasat
615  7$aF-104 aircraft.
615  7$aLaminar flow airfoils.
615  7$aFriction measurement.
615  7$aSkin friction.
615  7$aPressure distribution.
700   $aDrake$b Aaron$01417427
712 02$aAmes Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910704205203321
996   $aWing leading edge joint laminar flow tests$93525731
997   $aUNINA