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035   $a(EXLCZ)995470000002524086
100   $a20200623d1936      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe forces and moments on airplane engine mounts /$fby Philip Donely
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1936.
215   $a1 online resource (18 pages, 3 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 587
300   $a"December 1936."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 17).
606   $aAirplanes$xMotors
606   $aForce and energy$xMathematical models
606   $aMoments of inertia$xMathematical models
606   $aAirplanes$xMotors$2fast
615  0$aAirplanes$xMotors.
615  0$aForce and energy$xMathematical models.
615  0$aMoments of inertia$xMathematical models.
615  7$aAirplanes$xMotors.
700   $aDonely$b Philip$01390299
712 02$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   $a9910716608403321
996   $aThe forces and moments on airplane engine mounts$93512944
997   $aUNINA