01621ncm 2200493Ia 450 99639458710331620210104163556.0(CKB)3810000000008421(EEBO)2248566566(OCoLC)ocm58044221e(OCoLC)58044221(EXLCZ)99381000000000842120050304d1704 uy engurbn||||a|bb|A song[electronic resource] /sett by Mr. Iohn Weldon[London s.n.ca. 1704]1 score ([2] leaves)Song for high voice and continuo (figured bass).Caption title."The words by Capt. John Lawrance"--Head of leaf [2].First line: Reason, reason what art thou which the wise call great.Engraved throughout.From Congreve's The judgment of Paris.In: A collection of songs by severall masters / [collected by] Francis Norton.Reproduction of the original in the British Library.eebo-0018Songs (High voice) with continuoSongs, EnglishSongs (High voice) with continuo.Songs, English.Weldon John1676-1736.1007843Lawrence JohnCaptain.378098Congreve William1670-1729.163922Norton Francis1003498UMIUMIOCLCQOCLCGUMIBOOK996394587103316A song2424874UNISA00901nam a2200253 i 450099100049400970753620020506131208.0000309s1986 it ||| | ita b10708650-39ule_instEXGIL146673ExLDip.to Filol. Ling. e Lett.itaTessa, Delio156446Vecchia Europa /Delio Tessa ; a cura di Cristina Sacchi ; premessa di Angelo Stella[Milano] :Bompiani,[1986]196 p. ;22 cm.Nuova corona ;18Sacchi, CristinaStella, Angelo.b1070865023-02-1728-06-02991000494009707536LE008 FL.M. IX B 1812008000008185le008-E0.00-l- 00000.i1080439028-06-02Vecchia Europa912364UNISALENTOle00801-01-00ma -itait 0105165nam 2200601 450 991078724450332120230803210215.03-03826-616-7(CKB)3710000000281198(EBL)1910929(SSID)ssj0001407219(PQKBManifestationID)11799302(PQKBTitleCode)TC0001407219(PQKBWorkID)11409637(PQKB)10812371(Au-PeEL)EBL1910929(CaPaEBR)ebr10986829(OCoLC)899159194(MiAaPQ)EBC1910929(EXLCZ)99371000000028119820141201h20142014 uy| 0engur|n|---|||||txtccrAEROTECH V progressive aerospace research : selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia /edited by R. Varatharajoo [and four others]Switzerland :TTP,[2014]©20141 online resource (525 p.)Applied mechanics and materials,1660-9336 ;volume 629Description based upon print version of record.3-03835-232-2 Includes bibliographical references and index.AEROTECH V: Progressive Aerospace Research; Preface and Editorial Panel; Table of Contents; Chapter 1: Aerodynamics; Numerical Simulation of Noise Radiated from a Blunt Trailing Edge; Further Development of the Kinematic and Aerodynamic Modeling and Analysis of Flapping Wing Ornithopter from Basic Principles; Experimental Study on the Effect of Skin Flexibility on Aerodynamic Performance of Flapping Wings for Micro Air Vehicles; Visualization of Flow Field and Wake over Clean and Under-Loaded Wings; NACA 4415 Wing Modification Using Tubercles - A Numerical AnalysisComparison of Digital DATCOM and Wind Tunnel Data of a Winged Hybrid Airship's Generic ModelAn Experimental and Computational Fluid Dynamic Study of Axis-Symmetric Coanda Configuration for VTOL MAV Applications; Sensing Unsteady Pressure on MAV Wings: A New Method for Turbulence Alleviation; Chapter 2: Aerospace Structure; Multiple Crack Interactions in Bi-Material Plates under Mode I Tension Loading; Finite Element Computational Modeling and Simulation Studies of Non-Penetrating Impact Using Fundamental Principles; LCO Flutter Analysis on Coir Pressed Mat Fibre/Epoxy Composites PlateQuasi Static Analysis of a Biocomposite Aircraft RadomeModal Analysis of Thin Walled Multi-Cell Multi-Tapered Composite Beams of Closed Cross Sections; On the Dynamic Model of a Functionally Graded Spinning Structural Element of an Aircraft Appendage; Chapter 3: Propulsion; A Computational and Analytical Study into the Use of Counter-Flow Fluidic Thrust Vectoring Nozzle for Small Gas Turbine Engines; Computational Exploration of a Two-Spool High Bypass Turbofan Engine's Component Deterioration Effects on Engine Performance; CFD Validation and Analysis of a Single-Stage Axial CompressorAerodynamics Performance of Endwall Film Cooling under the Influence of Purge Flow in High Pressure Turbine CascadeSpray Characteristics of an Internal-Mix Airblast Atomizer; Computational Approach in Sizing of Pulsejet Engine; Chapter 4: Aerospace Design; Application of Coandă Jet for Generating Lift of Micro Air Vehicles - Preliminary Design Considerations; Performance Calculations within the Conceptual Design Process of Hand-Launched Aircraft; Conceptual Design of Flapping Wing Using Shape Memory Alloy Actuator for Micro Unmanned Aerial VehicleDesign and Analysis of an Aircraft Composite Hinge Bracket Using Finite Element ApproachReverse Engineering of a Fixed Wing Unmanned Aircraft 6-DoF Model for Navigation and Guidance Applications; Development of Blimp Platform for Aerial Photography; Autonomous Aerial Hard Docking of Fixed and Rotary Wing UAVs: Task Assessment and Solution Architecture; Aeroelastic Tailoring of Composite Wing Design Using Bee Colony Optimisation; Chapter 5: Aerospace System Performance; The Application of Multiple Vibration Neutralizers for Vibration Control in AircraftEffects of Aircraft Tail Configurations on Sensitivity to Yaw DisturbancesCollection of selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia. The 83 papers are grouped as follows: Chapter 1: Aerodynamics, Chapter 2: Aerospace Structure, Chapter 3: Propulsion, Chapter 4: Aerospace Design, Chapter 5: Aerospace System Performance, Chapter 6: Space Systems, Chapter 7: Avionics and Flight Management, Chapter 8: Aerospace Reviews, Chapter 9: Supporting Technologies for AerospaceApplied mechanics and materials ;v. 629.Space vehiclesCongressesSpace vehicles629.1323Varatharajoo R.MiAaPQMiAaPQMiAaPQBOOK9910787244503321AEROTECH V3684422UNINA