LEADER 01580oam  2200445I  450 
001 9910714090003321
005 20201211101825.0
035   $a(CKB)5470000002506769
035   $a(OCoLC)890696419
035   $a(EXLCZ)995470000002506769
100   $a20140916j196903    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExperimental pressure distributions on a 120° cone at Mach numbers from 2.96 to 4.63 and angles of attack from 0° to 20° /$fby Robert L. Stallings and Dorothy H. Tudor
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dMarch 1969.
215   $a1 online resource (76 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-5054
300   $a"March 1969."
320   $aIncludes bibliographical references (page 13).
606   $aAerodynamics$2nasat
606   $aMach number$2nasat
606   $aPressure distribution$2nasat
615  7$aAerodynamics.
615  7$aMach number.
615  7$aPressure distribution.
700   $aStallings$b Robert L.$01396665
702   $aTudor$b Dorothy H.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bCOP
801  2$bGPO
906   $aBOOK
912   $a9910714090003321
996   $aExperimental pressure distributions on a 120° cone at Mach numbers from 2.96 to 4.63 and angles of attack from 0° to 20$93457106
997   $aUNINA