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035   $a(OCoLC)1136490240
035   $a(EXLCZ)995470000002505070
100   $a20200116d1929      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWind tunnel pressure distribution tests on a series of biplane wing models$hPart I$iEffects of changes in stagger and gap /$fby Montgomery Knight and Richard W. Noyes
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1929.
215   $a1 online resource (13 pages, 20 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 310
300   $a"July, 1929."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 13).
517 3 $aEffects of changes in stagger and gap
606   $aAirplanes$xWings$xDesign and construction
606   $aWind tunnel testing
606   $aBiplanes
606   $aAirplanes$xWings$xDesign and construction$2fast
606   $aWind tunnel testing$2fast
615  0$aAirplanes$xWings$xDesign and construction.
615  0$aWind tunnel testing.
615  0$aBiplanes.
615  7$aAirplanes$xWings$xDesign and construction.
615  7$aWind tunnel testing.
700   $aKnight$b Montgomery$01390967
702   $aNoyes$b Richard W.
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   $a9910713862303321
996   $aWind tunnel pressure distribution tests on a series of biplane wing models$93444189
997   $aUNINA