LEADER 01829oam  2200493   450 
001 9910714049603321
005 20210317062536.0
035   $a(CKB)5470000002507151
035   $a(OCoLC)1136490317
035   $a(EXLCZ)995470000002507151
100   $a20200116d1930      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPerformance of a high-speed compression-ignition engine using multiple orifice fuel injection nozzles /$fby J.A. Spanogle and H.H. Foster
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1930.
215   $a1 online resource (18 pages, 21 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 344
300   $a"June, 1930."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 18).
606   $aAirplanes$xMotors$xFuel injection systems$xTesting
606   $aCombustion chambers$xTesting
606   $aCombustion chambers$xTesting$2fast
615  0$aAirplanes$xMotors$xFuel injection systems$xTesting.
615  0$aCombustion chambers$xTesting.
615  7$aCombustion chambers$xTesting.
700   $aSpanogle$b J. A.$01386736
702   $aFoster$b Hampton H.$f1894-
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
801  2$bSTF
801  2$bNJT
801  2$bGPO
906   $aBOOK
912   $a9910714049603321
996   $aPerformance of a high-speed compression-ignition engine using multiple orifice fuel injection nozzles$93512553
997   $aUNINA