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100   $a20190508d1957      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90° /$fby Jim A. Penland
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1957.
215   $a1 online resource (32 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 3861
300   $a"January 1957."
300   $a"Supersedes recently declassified NACA Research Memorandum L54A14 by Jim A. Penland, 1954"--Page 1.
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 13-14).
517 3 $aAerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to ninety degrees
606   $aCylinders$xAerodynamics
606   $aAerodynamic load
606   $aWind tunnel testing
606   $aHypersonic wind tunnels
606   $aAerodynamic load$2fast
606   $aCylinders$xAerodynamics$2fast
606   $aHypersonic wind tunnels$2fast
606   $aWind tunnel testing$2fast
615  0$aCylinders$xAerodynamics.
615  0$aAerodynamic load.
615  0$aWind tunnel testing.
615  0$aHypersonic wind tunnels.
615  7$aAerodynamic load.
615  7$aCylinders$xAerodynamics.
615  7$aHypersonic wind tunnels.
615  7$aWind tunnel testing.
700   $aPenland$b Jim A.$01416903
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bCOP
801  2$bTRAAL
801  2$bGPO
906   $aBOOK
912   $a9910713872803321
996   $aAerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90$93523799
997   $aUNINA