LEADER 02053oam  2200517   450 
001 9910716912503321
005 20211129142724.0
035   $a(CKB)5470000002527075
035   $a(OCoLC)1286629299
035   $a(EXLCZ)995470000002527075
100   $a20211129d1941      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWind-tunnel investigation of effect of yaw on lateral-stability characteristics$hIII$iSymmetrically tapered wing at various positions on circular fuselage with and without a vertical tail /$fby Isidore G. Recant and Arthur R. Wallace
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1941.
215   $a1 online resource (12 pages, 12 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 825
300   $a"September 1941."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 12).
517 3 $aSymmetrically tapered wing at various positions on circular fuselage with and without a vertical tail
606   $aAirplanes$xWings$xTesting
606   $aAirplanes$xFuselage
606   $aStability of airplanes
606   $aRolling (Aerodynamics)
606   $aYawing (Aerodynamics)
606   $aWind tunnel testing
615  0$aAirplanes$xWings$xTesting.
615  0$aAirplanes$xFuselage.
615  0$aStability of airplanes.
615  0$aRolling (Aerodynamics)
615  0$aYawing (Aerodynamics)
615  0$aWind tunnel testing.
700   $aRecant$b Isidore G.$01386872
702   $aWallace$b Arthur R.
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910716912503321
996   $aWind-tunnel investigation of effect of yaw on lateral-stability characteristics$93523012
997   $aUNINA