LEADER 01007nam 2200337Ia 450 001 996384875903316 005 20210903211306.0 035 $a(CKB)4940000000074344 035 $a(EEBO)2240926886 035 $a(OCoLC)ocm11958774e 035 $a(OCoLC)11958774 035 $a(EXLCZ)994940000000074344 100 $a19850424d1647 uy | 101 0 $aeng 135 $aurbn#|||a|bb| 200 14$aThe covntrie girle$b[electronic resource] $ea comedie, as it hath beene often acted with much applause /$fby T.B 210 $aLondon $cPrinted for A.R.$d1647 215 $a[84] p 300 $aAttributed to Anthony Brewer. Cf. BM. 300 $a"Never printed before" 300 $aReproduction of original in British Library. 330 $aeebo-0018 700 $aBrewer$b Anthony$factive 1630-1655.$0537643 801 0$bEAA 801 1$bEAA 801 2$bm/c 801 2$bWaOLN 906 $aBOOK 912 $a996384875903316 996 $aThe covntrie girle$92426304 997 $aUNISA LEADER 01845nam 2200517Ia 450 001 9910697003403321 005 20230902161802.0 035 $a(CKB)5470000002384873 035 $a(OCoLC)688604866 035 $a(EXLCZ)995470000002384873 100 $a20101202d2005 ua 0 101 0 $aeng 135 $aurmn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aLocal flow conditions for proplusion experiments on the F-15B Propulsion Flight Test Fixture$b[electronic resource] /$fMichael J. Vachon, Timothy R. Moes, Stephen Corda 210 1$aEdwards, Calif. :$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$d[2005] 215 $a1 online resource (28 pages) $cillustrations 225 1 $aNASA TM- ;$v2005-213670 300 $aTitle from title screen (viewed on Dec. 2, 2010). 300 $a"November 2005." 320 $aIncludes bibliographical references (page 11) 410 0$aNASA technical memorandum ;$v213670. 606 $aFlight tests$2nasat 606 $aMach number$2nasat 606 $aAngle of attack$2nasat 606 $aSupersonic speed$2nasat 606 $aSideslip$2nasat 606 $aNoses (forebodies)$2nasat 615 7$aFlight tests. 615 7$aMach number. 615 7$aAngle of attack. 615 7$aSupersonic speed. 615 7$aSideslip. 615 7$aNoses (forebodies) 700 $aVachon$b Michael J$01386041 701 $aMoes$b Timothy R$01386042 701 $aCorda$b Stephen$f1958-$01260554 712 02$aHugh L. Dryden Flight Research Center. 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910697003403321 996 $aLocal flow conditions for proplusion experiments on the F-15B Propulsion Flight Test Fixture$93434611 997 $aUNINA