LEADER 01691nam  2200505I  450 
001 9910702734603321
005 20150203132632.0
035   $a(CKB)5470000002430855
035   $a(OCoLC)902680759
035   $a(EXLCZ)995470000002430855
100   $a20150203j201408    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aData reduction functions for the Langley 14- by 22-foot subsonic tunnel /$fAndy D. Boney
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dAugust 2014.
215   $a1 online resource (iii, 77 pages)
225 1 $aNASA/TM ;$v2014-218513
300   $aTitle from title screen (viewed Feb. 3, 2015).
300   $a"August 2014."
320   $aIncludes bibliographical references (page 77).
606   $aData reduction$2nasat
606   $aSubsonic wind tunnels$2nasat
606   $aFlowmeters$2nasat
606   $aJet exhaust$2nasat
606   $aWall pressure$2nasat
606   $aLoads (forces)$2nasat
615  7$aData reduction.
615  7$aSubsonic wind tunnels.
615  7$aFlowmeters.
615  7$aJet exhaust.
615  7$aWall pressure.
615  7$aLoads (forces)
700   $aBoney$b Andy D.$01405267
702   $aNishikawa$b Hiroaki
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702734603321
996   $aData reduction functions for the Langley 14- by 22-foot subsonic tunnel$93481437
997   $aUNINA