LEADER 01572oam  2200445   450 
001 9910716910603321
005 20211130115610.0
035   $a(CKB)5470000002527094
035   $a(OCoLC)1154792965
035   $a(EXLCZ)995470000002527094
100   $a20200519d1939      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn experimental investigation of the normal acceleration of an airplane model in a gust /$fby Philip Donely
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1939.
215   $a1 online resource (15 pages, 21 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 706
300   $a"May 1939."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 15).
606   $aAirplanes$xModels$xWings$xTesting
606   $aGust loads
606   $aGust loads$2fast
615  0$aAirplanes$xModels$xWings$xTesting.
615  0$aGust loads.
615  7$aGust loads.
700   $aDonely$b Philip$01390299
712 02$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   $a9910716910603321
996   $aAn experimental investigation of the normal acceleration of an airplane model in a gust$93495931
997   $aUNINA