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001 9910714077203321
005 20201105145052.0
035   $a(CKB)5470000002506898
035   $a(OCoLC)761182042
035   $a(EXLCZ)995470000002506898
100   $a20111115j196811    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /$fby Charlie M. Jackson, Jr., Wallace C. Sawyer, and Rudeen S. Smith
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dNovember 1968.
215   $a1 online resource (102 pages) $cillustrations
225 1 $aNASA technical note ;$vNASA TN D-4865
300   $a"November 1968."
320   $aIncludes bibliographical references (page 52).
606   $aAerodynamic load
606   $aNoses (Space vehicles)$xTesting
606   $aAngle of attack (Aerodynamics)
606   $aAerodynamics, Supersonic$xTesting
615  0$aAerodynamic load.
615  0$aNoses (Space vehicles)$xTesting.
615  0$aAngle of attack (Aerodynamics)
615  0$aAerodynamics, Supersonic$xTesting.
700   $aJackson$b Charlie M.$01395048
702   $aSawyer$b Wallace C.
702   $aSmith$b Rudeen S.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910714077203321
996   $aA method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow$93519899
997   $aUNINA