LEADER 00799nam0-2200289---450- 001 990008522450403321 005 20071218163053.0 035 $a000852245 035 $aFED01000852245 035 $a(Aleph)000852245FED01 035 $a000852245 100 $a20070605d1963----km-y0itay50------ba 101 0 $aeng 102 $aGB 105 $ay-------001yy 200 1 $aLightweight concrete$fby Andrew Short and William Kinniburgh 210 $aLondon$cCR Books$dc1963 215 $aXIII, 368 p.$cill$d23 cm 700 1$aShort,$bAndrew$0305450 701 1$aKinniburgh,$bWilliam$0305451 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990008522450403321 952 $a08 AA 143$b1139 C.E.$fDINED 959 $aDINED 996 $aLightweight concrete$9733106 997 $aUNINA 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