LEADER 01695oam  2200481   450 
001 9910716611903321
005 20210727115156.0
035   $a(CKB)5470000002524051
035   $a(OCoLC)1159597583
035   $a(EXLCZ)995470000002524051
100   $a20200623d1936      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe reduction of aileron operating force by differential linkage /$fby Robert T. Jones and Albert I. Nerken
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1936.
215   $a1 online resource (13 pages, 10 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 586
300   $a"December 1936."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 13).
606   $aAilerons
606   $aAirplanes$xControl surfaces
606   $aAilerons$2fast
606   $aAirplanes$xControl surfaces$2fast
615  0$aAilerons.
615  0$aAirplanes$xControl surfaces.
615  7$aAilerons.
615  7$aAirplanes$xControl surfaces.
700   $aJones$b Robert T$g(Robert Thomas),$f1910-1999,$01409563
702   $aNerken$b Albert I.
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   $a9910716611903321
996   $aThe reduction of aileron operating force by differential linkage$93503272
997   $aUNINA