LEADER 02181oam  2200577   450 
001 9910715385503321
005 20210212100721.0
035   $a(CKB)5470000002510176
035   $a(OCoLC)1146215374
035   $a(EXLCZ)995470000002510176
100   $a20200326d1933      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of stabilizer location upon pitching and yawing moments in spins as shown by tests with the spinning balance /$fby M.J. Bamber and C.H. Zimmerman
210  1$aWashington [D.C.] :$cNational Advisory Committee for Aeronautics,$d1933.
215   $a1 online resource (11 pages, 8 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 474
300   $a"November, 1933."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 11).
606   $aAirplanes$xControl surfaces
606   $aAirplanes$xTail surfaces
606   $aPitching (Aerodynamics)$xMeasurement
606   $aYawing (Aerodynamics)$xMeasurement
606   $aSpin (Aerodynamics)
606   $aAirplanes$xControl surfaces$2fast
606   $aAirplanes$xTail surfaces$2fast
606   $aSpin (Aerodynamics)$2fast
615  0$aAirplanes$xControl surfaces.
615  0$aAirplanes$xTail surfaces.
615  0$aPitching (Aerodynamics)$xMeasurement.
615  0$aYawing (Aerodynamics)$xMeasurement.
615  0$aSpin (Aerodynamics)
615  7$aAirplanes$xControl surfaces.
615  7$aAirplanes$xTail surfaces.
615  7$aSpin (Aerodynamics)
700   $aBamber$b M. J.$01386953
702   $aZimmerman$b C. H.
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   $a9910715385503321
996   $aEffect of stabilizer location upon pitching and yawing moments in spins as shown by tests with the spinning balance$93497115
997   $aUNINA