LEADER 01898nam 2200409 n 450 001 996393687803316 005 20211115120742.0 035 $a(CKB)3810000000003934 035 $a(EEBO)2240885503 035 $a(UnM)99838664e 035 $a(UnM)99838664 035 $a(EXLCZ)993810000000003934 100 $a19901112d1596 uy | 101 0 $aeng 135 $aurbn#|||a|bb| 200 14$aThe pathvvay to musicke$b[electronic resource] $econtayning sundrie familiar and easie rules for the readie and true vnderstanding of the scale, or gamma-vt: vvherein is exactlie the shevved by plaine deffinitions, the principles of this arte, brieflie laide open by vvay of questions and answers, for the better instruction of the learner. Whereunto is annexed a treatise of descant, & certaine tables, vvhich doth teach hovv to remoue any song higher, or lovver from one key to another, neuer heretofore published 210 $aPrinted at London $c[By J. Danter] for William Barley, and are to be sold at his shop in Gratious streete neere Leaden-Hall$d1596 215 $a[52] p. $cmusic 300 $aEdited by William Barley?--STC. 300 $aPrinter's name from STC. 300 $aIntended to be issued with: Barley, William. A new booke of tabliture. (STC 1433). 300 $aSignatures: A-F? G² (G2 blank). 300 $aReproduction of the original in the British Library. 330 $aeebo-0018 606 $aMusic theory$xHistory$y16th century$9lat$2NLI 606 $aMusical intervals and scales$vEarly works to 1800$9lat$2NLI 615 7$aMusic theory$xHistory 615 7$aMusical intervals and scales 701 $aBarley$b William$fd. 1614.$01002655 801 0$bCu-RivES 801 1$bCu-RivES 801 2$bCStRLIN 801 2$bWaOLN 906 $aBOOK 912 $a996393687803316 996 $aThe pathvvay to musicke$92301284 997 $aUNISA LEADER 01996oam 2200565 450 001 9910706189103321 005 20170818150632.0 035 $a(CKB)5470000002454532 035 $a(OCoLC)703664188 035 $a(EXLCZ)995470000002454532 100 $a20110224j199902 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aFactors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft /$fW.G. Steenken [and three others] 210 1$aEdwards, California :$cNational Aeronautics and Space Administration, Dryden Flight Research Center$dFebruary 1999. 215 $a1 online resource (vii, 191 pages) $cillustrations 225 1 $aNASA/TM ;$v1999-206572 300 $a"February 1999." 300 $a"Performing organization: NASA Dryden Flight Research Center"--Report documentation page. 320 $aIncludes bibliographical references (page 34). 606 $aF-18 aircraft$2nasat 606 $aAerodynamic stability$2nasat 606 $aAngle of attack$2nasat 606 $aCompressors$2nasat 606 $aControl surfaces$2nasat 606 $aFlight control$2nasat 606 $aResearch vehicles$2nasat 606 $aRotors$2nasat 606 $aSubsonic speed$2nasat 615 7$aF-18 aircraft. 615 7$aAerodynamic stability. 615 7$aAngle of attack. 615 7$aCompressors. 615 7$aControl surfaces. 615 7$aFlight control. 615 7$aResearch vehicles. 615 7$aRotors. 615 7$aSubsonic speed. 700 $aSteenken$b William G.$01392405 712 02$aDryden Flight Research Facility, 801 0$bSSN 801 1$bSSN 801 2$bGPO 906 $aBOOK 912 $a9910706189103321 996 $aFactors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F$93502513 997 $aUNINA