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200 10$aAnno regni Gulielmi III. regis Angliae, Scotiae, Franciae & Hiberniae decimo & undecimo$b[electronic resource] $eAt the Parliament begun at Westminster the four and twentieth day of August, Anno Dom. 1698.  In the tenth year of the reign of our sovereign Lord William the third, by the grace of God, of England, Scotland, France and Ireland, king, defender of the faith, &c. and from thence continued by several prorogations to the sixth day of December, 1698. being the first session of this present Parliament
210   $aLondon $cPrinted by Charles Bill and the executrix of Thomas Newcomb, deceas'd; printers to the King's Most Excellent Majesty ;$aDublin $cAnd re-printed by John Brocas in School-House-Lane$dMDCXCIX. [1699]
215   $a[2], 6 p
300   $aReproduction of original in: Trinity College (Dublin, Ireland). Library.
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606   $aWool industry$xLaw and legislation$zGreat Britain$vEarly works to 1800
606   $aWool industry$xLaw and legislation$zIreland$vEarly works to 1800
606   $aExport controls$zGreat Britain$vSources
615  0$aWool industry$xLaw and legislation
615  0$aWool industry$xLaw and legislation
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712 02$aEngland and Wales.$bParliament.
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181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aStatic investigation of two STOL nozzle concepts with pitch thrust-vectoring capability /$fMary L. Mason and James R. Burley II
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dApril 1986.
215   $a1 online resource (54 pages) $cillustrations
225 1 $aNASA/TP ;$v2559
300   $a"April 1986."
320   $aIncludes bibliographical references (pages 13-14).
606   $aNozzle geometry$2nasat
606   $aStatic tests$2nasat
606   $aNozzle thrust coefficients$2nasat
606   $aAxisymmetric flow$2nasat
606   $aAfterburning$2nasat
606   $aJet nozzles$xTesting
606   $aAirplanes$xMotors$xThrust
606   $aPitching (Aerodynamics)
606   $aShort take-off and landing aircraft
606   $aAirplanes$xMotors$xThrust$2fast
606   $aJet nozzles$xTesting$2fast
606   $aPitching (Aerodynamics)$2fast
606   $aShort take-off and landing aircraft$2fast
608   $aOnline resources.
615  7$aNozzle geometry.
615  7$aStatic tests.
615  7$aNozzle thrust coefficients.
615  7$aAxisymmetric flow.
615  7$aAfterburning.
615  0$aJet nozzles$xTesting.
615  0$aAirplanes$xMotors$xThrust.
615  0$aPitching (Aerodynamics)
615  0$aShort take-off and landing aircraft.
615  7$aAirplanes$xMotors$xThrust.
615  7$aJet nozzles$xTesting.
615  7$aPitching (Aerodynamics)
615  7$aShort take-off and landing aircraft.
700   $aMason$b Mary L.$01407755
702   $aBurley$b James R.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
712 02$aLangley Research Center.
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