LEADER 01950oam  2200517   450 
001 9910716726903321
005 20210827133823.0
035   $a(CKB)5470000002524909
035   $a(OCoLC)1159597626
035   $a(EXLCZ)995470000002524909
100   $a20200623d1937      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMotion of the two-control airplane in rectilinear flight after initial disturbances with introduction of controls following an exponential law /$fby Alexander Klemin
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1937.
215   $a1 online resource (30 pages, 10 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 615
300   $a"September 1937."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 30).
606   $aStability of airplanes
606   $aAirplanes$xControl
606   $aEquations of motion
606   $aAirplanes$xControl$2fast
606   $aEquations of motion$2fast
606   $aStability of airplanes$2fast
615  0$aStability of airplanes.
615  0$aAirplanes$xControl.
615  0$aEquations of motion.
615  7$aAirplanes$xControl.
615  7$aEquations of motion.
615  7$aStability of airplanes.
700   $aKlemin$b Alexander$f1888-1950,$03489
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910716726903321
996   $aMotion of the two-control airplane in rectilinear flight after initial disturbances with introduction of controls following an exponential law$93454210
997   $aUNINA