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100   $a20190610d1935      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAnalysis of a strut with a single elastic support in the span, with applications to the design of airplane jury-strut systems /$fby A. Murray Schwartz, by Reid Bogert
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1935.
215   $a1 online resource (60 pages, 20 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 529
300   $a"May 1935."
300   $aThis note contains two separate parts: Part I - Derivation of formulas (A. Murray Schwartz) and Part II - Experimental investigation of formulas (Reid Bogert).
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references.
606   $aAeronautics$xResearch
606   $aAirplanes$xWings
606   $aAeronautics$xResearch$2fast
606   $aAirplanes$xWings$2fast
615  0$aAeronautics$xResearch.
615  0$aAirplanes$xWings.
615  7$aAeronautics$xResearch.
615  7$aAirplanes$xWings.
700   $aSchwartz$b A. Murray$01398363
702   $aBogert$b Reid
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
801  2$bSTF
801  2$bGPO
906   $aBOOK
912   $a9910713642703321
996   $aAnalysis of a strut with a single elastic support in the span, with applications to the design of airplane jury-strut systems$93461452
997   $aUNINA