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100   $a20170725j199805    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies /$fIrina G. Brykina, Carl D. Scott
210  1$aHouston, Texas :$cNational Aeronautics and Space Administration, Lyndon B. Johnson Space Center,$dMay 1998.
215   $a1 online resource (iv, 28 pages) $cillustrations
225 1 $aNASA/TM ;$v98-207890
300   $a"May 1998."
300   $a"Performing organization: Lyndon B. Johnson Space Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 15-16).
606   $aFlow measurement$2nasat
606   $aAxisymmetric flow$2nasat
606   $aAerodynamic heating$2nasat
606   $aParabolic bodies$2nasat
606   $aHypersonics$2nasat
606   $aAxisymmetric bodies$2nasat
606   $aBlunt bodies$2nasat
615  7$aFlow measurement.
615  7$aAxisymmetric flow.
615  7$aAerodynamic heating.
615  7$aParabolic bodies.
615  7$aHypersonics.
615  7$aAxisymmetric bodies.
615  7$aBlunt bodies.
700   $aBrykina$b Irina G.$01411056
702   $aScott$b Carl D.
712 02$aLyndon B. Johnson Space Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705868703321
996   $aAn approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies$93501247
997   $aUNINA