LEADER 02508oam 2200673I 450 001 9910713819203321 005 20200915142107.0 035 $a(CKB)5470000002505464 035 $a(OCoLC)1136490271 035 $a(EXLCZ)995470000002505464 100 $a20200116d1929 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aWind tunnel pressure distribution tests on a series of biplane wing models$hPart II$iEffects of changes in decalage, dihedral, sweepback and overhang /$fby Montgomery Knight and Richard W. Noyes 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1929. 215 $a1 online resource (6 pages, 32 unnumbered pages) $cillustrations 225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 325 300 $a"October, 1929." 300 $aIncludes errata. 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical reference (page 6). 517 3 $aEffects of changes in decalage, dihedral, sweepback and overhang 606 $aAirplanes$xDihedral wings 606 $aAirplanes$xModels$xTesting 606 $aAirplanes$xWings, Swept-back 606 $aAerodynamic load$xTesting 606 $aWind tunnel testing 606 $aBiplanes 606 $aAerodynamic load$xTesting$2fast 606 $aAirplanes$xDihedral wings$2fast 606 $aAirplanes$xModels$xTesting$2fast 606 $aAirplanes$xWings, Swept-back$2fast 606 $aWind tunnel testing$2fast 615 0$aAirplanes$xDihedral wings. 615 0$aAirplanes$xModels$xTesting. 615 0$aAirplanes$xWings, Swept-back. 615 0$aAerodynamic load$xTesting. 615 0$aWind tunnel testing. 615 0$aBiplanes. 615 7$aAerodynamic load$xTesting. 615 7$aAirplanes$xDihedral wings. 615 7$aAirplanes$xModels$xTesting. 615 7$aAirplanes$xWings, Swept-back. 615 7$aWind tunnel testing. 700 $aKnight$b Montgomery$01390967 702 $aNoyes$b Richard W. 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bOCLCO 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910713819203321 996 $aWind tunnel pressure distribution tests on a series of biplane wing models$93444189 997 $aUNINA