LEADER 02005oam  2200553   450 
001 9910715127903321
005 20201228124219.0
035   $a(CKB)5470000002508737
035   $a(OCoLC)1139565351
035   $a(EXLCZ)995470000002508737
100   $a20200206d1931      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cn$2rdamedia
183   $anc$2rdacarrier
200 10$aPerformance of a compression-ignition engine with a precombustion chamber having high-velocity air flow /$fby J.A. Spanogle and C.S. Moore
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1931.
215   $a1 online resource (15 pages, 14 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 396
300   $a"October, 1931."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 15).
606   $aCombustion chambers
606   $aInternal combustion engines$xCombustion$xTesting
606   $aFuel
606   $aAerosols
606   $aInjectors
606   $aCombustion chambers$2fast
606   $aInternal combustion engines$xCombustion$xTesting$2fast
615  0$aCombustion chambers.
615  0$aInternal combustion engines$xCombustion$xTesting.
615  0$aFuel.
615  0$aAerosols.
615  0$aInjectors.
615  7$aCombustion chambers.
615  7$aInternal combustion engines$xCombustion$xTesting.
700   $aSpanogle$b J. A.$01386736
702   $aMoore$b C. S.
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   $a9910715127903321
996   $aPerformance of a compression-ignition engine with a precombustion chamber having high-velocity air flow$93523297
997   $aUNINA