LEADER 01717oam  2200517   450 
001 9910713430503321
005 20200814124001.0
035   $a(CKB)5470000002501351
035   $a(OCoLC)1121047362
035   $a(EXLCZ)995470000002501351
100   $a20190926d1923      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aReduction in efficiency of propellers due to slipstream /$fby Max M. Munk
210  1$a[Washington, D.C.] :$cNational Advisory Committee for Aeronautics,$d1923.
215   $a1 online resource (6 pages)
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 170
300   $a"December 1923."
300   $a"From Technische Berichte, Vol. III, No. 7."
300   $a"Translated by National Advisory Committee for Aeronautics"--Page 6.
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical reference (page 1).
606   $aPropellers, Aerial
606   $aAir flow
606   $aAir flow$2fast
606   $aPropellers, Aerial$2fast
615  0$aPropellers, Aerial.
615  0$aAir flow.
615  7$aAir flow.
615  7$aPropellers, Aerial.
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   $a9910713430503321
996   $aReduction in efficiency of propellers due to slipstream$93528986
997   $aUNINA