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200 1 $aQuattro lezioni di tecnologia dell'architettura$fRaffaella Crespi
205   $a3. ed
210   $aMilano$cF. Angeli$dcopyr. 1985
215   $a156 p.$cill., fot.$d21 cm
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410  0$10010023240$12001$aRicerche di tecnologia dell'architettura$fcollana diretta da Raffaella Crespi e Guido Nardi
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996   $aQuattro lezioni di tecnologia dell'architettura$9327043
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101 0 $aeng
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181   $ctxt$2rdacontent
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200 12$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,
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996   $aA method for calculating the aerodynamic loading on wing-body combinations at small angles of attack in supersonic flow$93544295
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