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100   $a20111122j197912    ua             0
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181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic characteristics of a hypersonic research airplane concept having a 70 ?swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 /$fJim A. Penland, James B. Hallissy, and James L. Dillon
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dDecember 1979.
215   $a1 online resource (144 pages) $cillustrations
225 1 $aNASA technical paper ;$v1552
300   $aTitle from title screen (viewed Sept. 22, 2014).
300   $a"December 1979."
300   $a"Performing organization, NASA Langley Research Center"--Technical report documentation page.
320   $aIncludes bibliographical references (pages 20-22).
606   $aAerodynamics
606   $aAerodynamic characteristics$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aDelta wings$2nasat
606   $aHypersonic aircraft$2nasat
606   $aWind tunnel tests$2nasat
606   $aAerodynamics$2fast
615  0$aAerodynamics.
615  7$aAerodynamic characteristics.
615  7$aComputational fluid dynamics.
615  7$aDelta wings.
615  7$aHypersonic aircraft.
615  7$aWind tunnel tests.
615  7$aAerodynamics.
700   $aPenland$b Jim A.$01416903
702   $aHallissy$b James B.
702   $aDillon$b James L.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910702683003321
996   $aAerodynamic characteristics of a hypersonic research airplane concept having a 70 ?swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0$93525942
997   $aUNINA