LEADER 01719oam  2200493   450 
001 9910713543003321
005 20200526105000.0
035   $a(CKB)5470000002502234
035   $a(OCoLC)1127388903
035   $a(EXLCZ)995470000002502234
100   $a20191113d1926      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPropeller design$hI$iPractical application of the blade element theory /$fby Fred E. Weick
210  1$a[Washington, D.C.] :$cNational Advisory Committee for Aeronautics,$d1926.
215   $a1 online resource (14 pages, 7 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 235
300   $a"May 1926."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 10).
517 3 $aPractical application of the blade element theory
606   $aPropellers$xDesign and construction
606   $aPropellers, Aerial
606   $aPropellers, Aerial$2fast
606   $aPropellers$xDesign and construction$2fast
615  0$aPropellers$xDesign and construction.
615  0$aPropellers, Aerial.
615  7$aPropellers, Aerial.
615  7$aPropellers$xDesign and construction.
700   $aWeick$b Fred E.$01387817
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910713543003321
996   $aPropeller design$93444943
997   $aUNINA