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001 9910713805003321
005 20200918141415.0
035   $a(CKB)5470000002505607
035   $a(OCoLC)1136490288
035   $a(EXLCZ)995470000002505607
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$hPart III$iEffects of changes in various combinations of stagger, gap, sweepback, and decalage /$fby Montgomery Knight and Richard W. Noyes
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1929.
215   $a1 online resource (6 pages, 22 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 330
300   $a"December, 1929."
300   $aIncludes errata.
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 6).
517 3 $aEffects of changes in various combinations of stagger, gap, sweepback, and decalage
606   $aAerodynamic load$xTesting
606   $aAirplanes$xModels$xTesting
606   $aAirplanes$xWings, Swept-back
606   $aWind tunnel testing
606   $aBiplanes
606   $aAerodynamic load$xTesting$2fast
606   $aAirplanes$xModels$xTesting$2fast
606   $aAirplanes$xWings, Swept-back$2fast
606   $aWind tunnel testing$2fast
615  0$aAerodynamic load$xTesting.
615  0$aAirplanes$xModels$xTesting.
615  0$aAirplanes$xWings, Swept-back.
615  0$aWind tunnel testing.
615  0$aBiplanes.
615  7$aAerodynamic load$xTesting.
615  7$aAirplanes$xModels$xTesting.
615  7$aAirplanes$xWings, Swept-back.
615  7$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   $a9910713805003321
996   $aWind tunnel pressure distribution tests on a series of biplane wing models$93444189
997   $aUNINA