LEADER 02022oam  2200541   450 
001 9910716869403321
005 20210922134045.0
035   $a(CKB)5470000002525490
035   $a(OCoLC)1159597668
035   $a(EXLCZ)995470000002525490
100   $a20200623d1938      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA flight investigation of the reduction of aileron operating force by means of fixed tabs and differential linkage, with notes on linkage design /$fby H.A. Soule? and James A. Hootman
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1938.
215   $a1 online resource (12 pages, 12 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 653
300   $a"June 1938."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 12).
606   $aAilerons
606   $aAirplanes$xFlight testing
606   $aAeronautics$xResearch
606   $aAeronautics$xResearch$2fast
606   $aAilerons$2fast
606   $aAirplanes$xFlight testing$2fast
615  0$aAilerons.
615  0$aAirplanes$xFlight testing.
615  0$aAeronautics$xResearch.
615  7$aAeronautics$xResearch.
615  7$aAilerons.
615  7$aAirplanes$xFlight testing.
700   $aSoule$b Hartley A$g(Hartley Akin),$f1904-1988,$01399820
702   $aHootman$b James A.
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bTRAAL
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910716869403321
996   $aA flight investigation of the reduction of aileron operating force by means of fixed tabs and differential linkage, with notes on linkage design$93521784
997   $aUNINA