LEADER 01885oam  2200529I  450 
001 9910713818903321
005 20200915143446.0
035   $a(CKB)5470000002505467
035   $a(OCoLC)1136490256
035   $a(EXLCZ)995470000002505467
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 an airfoil with trailing edge flap /$fby Carl J. Wenzinger and Oscar Loeser, Jr
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1929.
215   $a1 online resource (10 pages, 12 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 326
300   $a"October, 1929."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (pages 7-8).
606   $aAerofoils
606   $aFlaps (Airplanes)
606   $aWind tunnel testing
606   $aAerodynamic load$xTesting
606   $aAerodynamic load$xTesting$2fast
606   $aWind tunnel testing$2fast
615  0$aAerofoils.
615  0$aFlaps (Airplanes)
615  0$aWind tunnel testing.
615  0$aAerodynamic load$xTesting.
615  7$aAerodynamic load$xTesting.
615  7$aWind tunnel testing.
700   $aWenzinger$b Carl J$g(Carl Joseph),$f1903-1988,$01386955
702   $aLoeser$b Oscar$cJr.,
712 02$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   $a9910713818903321
996   $aWind tunnel pressure distribution tests on an airfoil with trailing edge flap$93487002
997   $aUNINA