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100   $a20200615d1941      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe theoretical lateral motions of an automatically controlled airplane subjected to a yawing-moment disturbance /$fby Frederick H. Imlay
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1941.
215   $a1 online resource (16 pages, 7 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vno. 809
300   $a"June 1941."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 16).
606   $aAirplanes$xControl
606   $aAutomatic pilot (Airplanes)
606   $aStability of airplanes
606   $aYawing (Aerodynamics)
606   $aAirplanes$xControl$2fast
606   $aAutomatic pilot (Airplanes)$2fast
606   $aStability of airplanes$2fast
606   $aYawing (Aerodynamics)$2fast
615  0$aAirplanes$xControl.
615  0$aAutomatic pilot (Airplanes)
615  0$aStability of airplanes.
615  0$aYawing (Aerodynamics)
615  7$aAirplanes$xControl.
615  7$aAutomatic pilot (Airplanes)
615  7$aStability of airplanes.
615  7$aYawing (Aerodynamics)
700   $aImlay$b Frederick H.$01386951
712 02$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   $a9910717251603321
996   $aThe theoretical lateral motions of an automatically controlled airplane subjected to a yawing-moment disturbance$93499802
997   $aUNINA