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200 1 $a<<The>> physical theory of neutron chain reactors$fAlvin M. Weinberg, Eugene P. Wigner
210   $aChicago$cThe University of Chicago press$d1958
215   $aXII, 801 p.$cill.$d25 cm
606 0 $aFisica nucleare
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700  1$aWEINBERG,$bAlvin M.$0605925
701  1$aWIGNER,$bEugene P.$0462233
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996   $aPhysical theory of neutron chain reactors$91121137
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100   $a20110224d2009      ua             0
101 0 $aeng
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181   $ctxt$2rdacontent
182   $cc$2rdamedia
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200 10$aCFD analysis of nozzle jet plume effects on sonic boom signature$b[electronic resource] /$fTrong T. Bui
210  1$aEdwards, Calif. :$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$d[2009]
215   $a1 online resource (40 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2009-214650
300   $aTitle from title screen (viewed on May 14, 2012).
300   $a"September 2009."
300   $aIncludes errata sheet.
320   $aIncludes bibliographical references (page 40).
410  0$aNASA technical memorandum ;$v2009-214650.
517 3 $aComputational fluid dynamics analysis of nozzle jet plume effects on sonic boom signature
606   $aComputational fluid dynamics$2nasat
606   $aNozzle flow$2nasat
606   $aGas jets$2nasat
606   $aNozzle geometry$2nasat
606   $aSonic booms$2nasat
606   $aWind tunnel tests$2nasat
606   $aPlumes$2nasat
606   $aF-15 aircraft$2nasat
615  7$aComputational fluid dynamics.
615  7$aNozzle flow.
615  7$aGas jets.
615  7$aNozzle geometry.
615  7$aSonic booms.
615  7$aWind tunnel tests.
615  7$aPlumes.
615  7$aF-15 aircraft.
700   $aBui$b Trong T$01390450
701   $aBui$b Trong T$01390450
712 02$aNASA Dryden Flight Research Center.
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996   $aCFD analysis of nozzle jet plume effects on sonic boom signature$93531194
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