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100   $a20191113d1926      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effect of tube length upon the recorded pressures from a pair of static orifices in a wing panel /$fby T. Carroll and R.E. Mixon
210  1$a[Washington, D.C.] :$cNational Advisory Committee for Aeronautics,$d1926.
215   $a1 online resource (4 pages, 1 unnumbered page) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 251
300   $a"November 1926."
300   $aNo Federal Depository Library Program (FDLP) item number.
606   $aPressure$xMeasurement
606   $aAir pressure$xMeasurement
606   $aHoles
606   $aAir pressure$xMeasurement$2fast
606   $aHoles$2fast
606   $aPressure$xMeasurement$2fast
615  0$aPressure$xMeasurement.
615  0$aAir pressure$xMeasurement.
615  0$aHoles.
615  7$aAir pressure$xMeasurement.
615  7$aHoles.
615  7$aPressure$xMeasurement.
700   $aCarroll$b Thomas$01381230
702   $aMixon$b R. E.
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910713527803321
996   $aThe effect of tube length upon the recorded pressures from a pair of static orifices in a wing panel$93460375
997   $aUNINA