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035   $a(EXLCZ)995470000002504825
100   $a20190610d1954      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic forces, moments, and stability derivatives for slender bodies of general cross section /$fby Alvin H. Sacks
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1954.
215   $a1 online resource (74 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 3283
300   $a"November 1954."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (pages 53-54).
606   $aAerodynamics
606   $aAirplanes
606   $aMathematical analysis
606   $aStability of airplanes
606   $aAerodynamics$2fast
606   $aAirplanes$2fast
606   $aMathematical analysis$2fast
606   $aStability of airplanes$2fast
615  0$aAerodynamics.
615  0$aAirplanes.
615  0$aMathematical analysis.
615  0$aStability of airplanes.
615  7$aAerodynamics.
615  7$aAirplanes.
615  7$aMathematical analysis.
615  7$aStability of airplanes.
700   $aSacks$b Alvin H.$01399803
712 02$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   $a9910713886503321
996   $aAerodynamic forces, moments, and stability derivatives for slender bodies of general cross section$93465730
997   $aUNINA