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200 03$aAn account of Sir George Rooke's arrival in the chanel, with the fleet under his command$b[electronic resource]
210   $aIn the Savoy [London] $cPrinted by Edward Jones$d1696
215   $a1 sheet ([1] p.)
300   $aDated: "Whitehall April 24. 1696."
300   $aReproduction of original in: National Library of Scotland.
330   $aeebo-0097
606   $aGreat Britain$xHistory, Naval$yStuarts, 1603-1714
608   $aBroadsides$zEngland$y17th century.$2rbgenr
615  0$aGreat Britain$xHistory, Naval
701   $aRooke$b George$cSir,$f1650-1709.$01007508
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912   $a996387158703316
996   $aAn account of Sir George Rooke's arrival in the chanel, with the fleet under his command$92367746
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100   $a20190610d1950      ua             0
101 0 $aeng
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181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAnalysis for control application of dynamic characteristics of turbojet engine with tail-pipe burning /$fby Melvin S. Feder and Richard Hood
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1950.
215   $a1 online resource (39 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 2183
300   $a"September 1950."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 35).
606   $aAirplanes$xControl systems
606   $aAirplanes$xTurbine-propeller engines
606   $aAirplanes$xTurbofan engines$xAfterburners
606   $aMathematical analysis
606   $aTransfer functions
606   $aAirplanes$xControl systems$2fast
606   $aAirplanes$xTurbine-propeller engines$2fast
606   $aAirplanes$xTurbofan engines$xAfterburners$2fast
606   $aMathematical analysis$2fast
606   $aTransfer functions$2fast
615  0$aAirplanes$xControl systems.
615  0$aAirplanes$xTurbine-propeller engines.
615  0$aAirplanes$xTurbofan engines$xAfterburners.
615  0$aMathematical analysis.
615  0$aTransfer functions.
615  7$aAirplanes$xControl systems.
615  7$aAirplanes$xTurbine-propeller engines.
615  7$aAirplanes$xTurbofan engines$xAfterburners.
615  7$aMathematical analysis.
615  7$aTransfer functions.
700   $aFeder$b Melvin S.$01409838
702   $aHood$b Richard
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
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906   $aBOOK
912   $a9910713754903321
996   $aAnalysis for control application of dynamic characteristics of turbojet engine with tail-pipe burning$93497317
997   $aUNINA