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100   $a20190610d1949      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic properties of cruciform-wing and body combinations at subsonic, transonic, and supersonic speeds /$fby John R. Spreiter
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1949.
215   $a1 online resource (32 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 1897
300   $a"June 1949."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 30).
606   $aAerodynamic load
606   $aAerodynamics
606   $aAirplanes$xWings
606   $aAerodynamic load$2fast
606   $aAerodynamics$2fast
606   $aAirplanes$xWings$2fast
615  0$aAerodynamic load.
615  0$aAerodynamics.
615  0$aAirplanes$xWings.
615  7$aAerodynamic load.
615  7$aAerodynamics.
615  7$aAirplanes$xWings.
700   $aSpreiter$b John R.$01389691
712 02$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   $a9910713762903321
996   $aAerodynamic properties of cruciform-wing and body combinations at subsonic, transonic, and supersonic speeds$93462006
997   $aUNINA