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100   $a20120408j197110    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA method for calculating the aerodynamic loading on wing-body combinations at small angles of attack in supersonic flow /$fby Charles M. Jackson, Jr. and Wallace C. Sawyer
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dOctober 1971.
215   $a1 online resource (32 pages) $cillustrations
225 1 $aNASA/TN ;$vD-6441
300   $a"October 1971."
320   $aIncludes bibliographical references (page 12).
606   $aAerodynamics$2nasat
606   $aInterference$2nasat
606   $aAerodynamics, Supersonic$2fast
606   $aInterference (Aerodynamics)$2fast
615  7$aAerodynamics.
615  7$aInterference.
615  7$aAerodynamics, Supersonic.
615  7$aInterference (Aerodynamics)
700   $aJackson$b Charlie M.$01395048
702   $aSawyer$b Wallace C.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bTRL
801  2$bAD#
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910715360203321
996   $aA method for calculating the aerodynamic loading on wing-body combinations at small angles of attack in supersonic flow$93544295
997   $aUNINA