LEADER 02076oam  2200577   450 
001 9910713894003321
005 20200820113958.0
035   $a(CKB)5470000002504750
035   $a(OCoLC)1104148302
035   $a(EXLCZ)995470000002504750
100   $a20190610d1952      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAirfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range /$fby Dean R. Chapman
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1952.
215   $a1 online resource (44 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 2787
300   $a"September 17, 1952."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 24).
606   $aAerodynamic load
606   $aAerodynamics, Supersonic
606   $aAerofoils
606   $aDrag (Aerodynamics)
606   $aAerodynamic load$2fast
606   $aAerodynamics, Supersonic$2fast
606   $aAerofoils$2fast
606   $aDrag (Aerodynamics)$2fast
615  0$aAerodynamic load.
615  0$aAerodynamics, Supersonic.
615  0$aAerofoils.
615  0$aDrag (Aerodynamics)
615  7$aAerodynamic load.
615  7$aAerodynamics, Supersonic.
615  7$aAerofoils.
615  7$aDrag (Aerodynamics)
700   $aChapman$b Dean R.$01401174
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bTRAAL
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910713894003321
996   $aAirfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range$93493800
997   $aUNINA