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001 9910713877203321
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035   $a(CKB)5470000002504919
035   $a(OCoLC)1104148280
035   $a(EXLCZ)995470000002504919
100   $a20190610d1956      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base /$fby Eugene S. Love
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1956.
215   $a1 online resource (62 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 3709
300   $a"September 1956."
300   $a"Supersedes recently declassified NACA Research Memorandum L9K09 by Eugene S. Love, 1950"--Page 1.
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (pages 25-26).
606   $aAerodynamic load
606   $aAerodynamics, Supersonic
606   $aBody of revolution
606   $aAerodynamic load$2fast
606   $aAerodynamics, Supersonic$2fast
606   $aBody of revolution$2fast
615  0$aAerodynamic load.
615  0$aAerodynamics, Supersonic.
615  0$aBody of revolution.
615  7$aAerodynamic load.
615  7$aAerodynamics, Supersonic.
615  7$aBody of revolution.
700   $aLove$b Eugene S.$01421137
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bTRAAL
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910713877203321
996   $aAerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base$93541633
997   $aUNINA