LEADER 02004oam  2200565   450 
001 9910713358403321
005 20200401074906.0
035   $a(CKB)5470000002500059
035   $a(OCoLC)1111633657
035   $a(EXLCZ)995470000002500059
100   $a20190806d1923      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals /$fby Max M. Munk
210  1$a[Washington, D.C.] :$cNational Advisory Committee for Aeronautics,$d1923.
215   $a1 online resource (9 pages, 2 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 122
300   $a"January, 1923."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 1).
606   $aLift (Aerodynamics)
606   $aAngle of attack (Aerodynamics)
606   $aAerofoils
606   $aCamber (Aerofoils)
606   $aAerofoils$2fast
606   $aAngle of attack (Aerodynamics)$2fast
606   $aCamber (Aerofoils)$2fast
606   $aLift (Aerodynamics)$2fast
615  0$aLift (Aerodynamics)
615  0$aAngle of attack (Aerodynamics)
615  0$aAerofoils.
615  0$aCamber (Aerofoils)
615  7$aAerofoils.
615  7$aAngle of attack (Aerodynamics)
615  7$aCamber (Aerofoils)
615  7$aLift (Aerodynamics)
700   $aMunk$b Max M$g(Max Michael),$f1890-$01386130
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCF
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910713358403321
996   $aThe determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals$93526198
997   $aUNINA