LEADER 01774oam  2200529   450 
001 9910713072903321
005 20200617082549.0
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035   $a(OCoLC)1111581289
035   $a(EXLCZ)995470000002499472
100   $a20190805d1922      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNotes on propeller design$hIII$iThe aerodynamical equations of the propeller blade elements /$fby Max M. Munk
210  1$a[Washington D.C.] :$cNational Advisory Committee for Aeronautics,$d1922.
215   $a1 online resource (10 pages) $cillustration
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 95
300   $a"May, 1922."
300   $aNo Federal Depository Library Program (FDLP) item number.
606   $aPropellers, Aerial
606   $aPropellers, Aerial$xDesign and construction
606   $aAir flow
606   $aAir flow$2fast
606   $aPropellers, Aerial$2fast
606   $aPropellers, Aerial$xDesign and construction$2fast
615  0$aPropellers, Aerial.
615  0$aPropellers, Aerial$xDesign and construction.
615  0$aAir flow.
615  7$aAir flow.
615  7$aPropellers, Aerial.
615  7$aPropellers, Aerial$xDesign and construction.
700   $aMunk$b Max M$g(Max Michael),$f1890-$01386130
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
801  2$bSTF
801  2$bGPO
906   $aBOOK
912   $a9910713072903321
996   $aNotes on propeller design$93441525
997   $aUNINA