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035   $a(EXLCZ)995470000002501178
100   $a20190909d1923      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCalculations for a single-strut biplane with reference to the tensions in the wing bracing /$fby O. Blumenthal
210  1$a[Washington, D.C.] :$cNational Advisory Committee for Aeronautics,$d1923.
215   $a1 online resource (28 pages, 3 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 143
300   $a"June 1923."
300   $a"From Technische Berichte, Vol. III, No. 5."
300   $a"Translated by National Advisory Committee for Aeronautics"--Page 28.
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references.
606   $aAirplanes$xWings
606   $aStrains and stresses
606   $aStruts (Engineering)
606   $aMathematical models
606   $aAirplanes$xWings$2fast
606   $aMathematical models$2fast
606   $aStrains and stresses$2fast
606   $aStruts (Engineering)$2fast
615  0$aAirplanes$xWings.
615  0$aStrains and stresses.
615  0$aStruts (Engineering)
615  0$aMathematical models.
615  7$aAirplanes$xWings.
615  7$aMathematical models.
615  7$aStrains and stresses.
615  7$aStruts (Engineering)
700   $aBlumenthal$b Otto$f1876-1944,$054552
712 02$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   $a9910713447603321
996   $aCalculations for a single-strut biplane with reference to the tensions in the wing bracing$93528994
997   $aUNINA