LEADER 01849oam  2200469I  450 
001 9910712842603321
005 20200131105329.0
035   $a(CKB)5470000002497758
035   $a(OCoLC)1107323707
035   $a(EXLCZ)995470000002497758
100   $a20190703d1921      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMeasurements of rudder moments on an airplane during flight /$fby v. Heidelberg
210  1$a[Washington, D.C.] :$cNational Advisory Committee for Aeronautics,$d1921.
215   $a1 online resource (23 pages, 5 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 38
300   $a"January, 1921."
300   $a"Translated from Zeitschrift fu?r Flugtechnik und Motorluftschiffahrt, Volumes Nos. 21 and 22, Paris Office, N.A.C.A."
300   $aAuthor is listed as "Ing. v. Heidelberg", however, this may not be a single author, but could signify "engineers from Heidelberg."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references.
606   $aAirplanes$xSteering-gear$xTesting
606   $aAirplanes$xTail surfaces
606   $aAirplanes$xTail surfaces$2fast
615  0$aAirplanes$xSteering-gear$xTesting.
615  0$aAirplanes$xTail surfaces.
615  7$aAirplanes$xTail surfaces.
700   $aHeidelberg$b V.$01394023
712 02$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   $a9910712842603321
996   $aMeasurements of rudder moments on an airplane during flight$93457759
997   $aUNINA