LEADER 01937oam  2200529   450 
001 9910715249003321
005 20210125141947.0
035   $a(CKB)5470000002509534
035   $a(OCoLC)1143006536
035   $a(EXLCZ)995470000002509534
100   $a20200304d1932      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effect of connecting-passage diameter on the performance of a compression-ignition engine with a precombustion chamber /$fby C.S. Moore and J.H. Collins, Jr
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1932.
215   $a1 online resource (14 pages, 16 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 436
300   $a"November, 1932."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 14).
606   $aDiesel motor$xTesting
606   $aCombustion chambers
606   $aFuel$xCombustion
606   $aCombustion chambers$2fast
606   $aDiesel motor$xTesting$2fast
606   $aFuel$xCombustion$2fast
615  0$aDiesel motor$xTesting.
615  0$aCombustion chambers.
615  0$aFuel$xCombustion.
615  7$aCombustion chambers.
615  7$aDiesel motor$xTesting.
615  7$aFuel$xCombustion.
700   $aMoore$b C. S.$01387423
702   $aCollins$b J. H.$cJr.,
712 02$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   $a9910715249003321
996   $aThe effect of connecting-passage diameter on the performance of a compression-ignition engine with a precombustion chamber$93530791
997   $aUNINA