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200 1 $aMuri, Infissi e Ossature$eelementi costruttivi verticali$fCh. Mondin$gGiovanni Emilio Buzzelli
210   $aBologna$cC.E.L.I.$d1963
215   $a647 p.$dill.$d18 cm
300   $aTit. orig.: Aide-Mèmoire Trad. da:Buzzelli Giovanni Emilio
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702  1$aBuzzelli,$bGiovanni Emilio
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181   $ctxt$2rdacontent
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200 10$aAerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes /$fRobert J. Nowak, Cindy W. Albertson, and L. Roane Hunt
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dJanuary 1985.
215   $a1 online resource (87 pages) $cillustrations
225 1 $aNASA/TP ;$v2345
300   $a"January 1985."
300   $aPrepared at Langley Research Center.
320   $aIncludes bibliographical references (pages 19-21).
606   $aFlow distribution$2nasat
606   $aCones$2nasat
606   $aAerodynamic heating$2nasat
606   $aBoundary layer transition$2nasat
606   $aTurbulent boundary layer$2nasat
606   $aAngle of attack (Aerodynamics)
606   $aNoses (Aircraft)
606   $aReynolds number
606   $aAerothermodynamics
606   $aAerothermodynamics$2fast
606   $aAngle of attack (Aerodynamics)$2fast
606   $aNoses (Aircraft)$2fast
606   $aReynolds number$2fast
615  7$aFlow distribution.
615  7$aCones.
615  7$aAerodynamic heating.
615  7$aBoundary layer transition.
615  7$aTurbulent boundary layer.
615  0$aAngle of attack (Aerodynamics)
615  0$aNoses (Aircraft)
615  0$aReynolds number.
615  0$aAerothermodynamics.
615  7$aAerothermodynamics.
615  7$aAngle of attack (Aerodynamics)
615  7$aNoses (Aircraft)
615  7$aReynolds number.
700   $aNowak$b Robert J.$01401795
702   $aAlbertson$b Cindy W.
702   $aHunt$b L. Roane$g(Lewis Roane),
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
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