LEADER 05199nam 2200613 450 001 9910459893603321 005 20200520144314.0 010 $a3-03826-616-7 035 $a(CKB)3710000000281198 035 $a(EBL)1910929 035 $a(SSID)ssj0001407219 035 $a(PQKBManifestationID)11799302 035 $a(PQKBTitleCode)TC0001407219 035 $a(PQKBWorkID)11409637 035 $a(PQKB)10812371 035 $a(MiAaPQ)EBC1910929 035 $a(Au-PeEL)EBL1910929 035 $a(CaPaEBR)ebr10986829 035 $a(OCoLC)899159194 035 $a(EXLCZ)993710000000281198 100 $a20141201h20142014 uy| 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aAEROTECH V $eprogressive aerospace research : selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia /$fedited by R. Varatharajoo [and four others] 210 1$aSwitzerland :$cTTP,$d[2014] 210 4$dİ2014 215 $a1 online resource (525 p.) 225 1 $aApplied mechanics and materials,$x1660-9336 ;$vvolume 629 300 $aDescription based upon print version of record. 311 $a3-03835-232-2 320 $aIncludes bibliographical references and index. 327 $aAEROTECH 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 Analysis 327 $aComparison 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 Plate 327 $aQuasi 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 Compressor 327 $aAerodynamics 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 Coanda? 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 Vehicle 327 $aDesign 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 Aircraft 327 $aEffects of Aircraft Tail Configurations on Sensitivity to Yaw Disturbances 330 $aCollection of selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia. The 83 papers are grouped as follows: Chapter 1: Aerodynamics, Chapter 2: Aerospace Structure, Chapter 3: Propulsion, Chapter 4: Aerospace Design, Chapter 5: Aerospace System Performance, Chapter 6: Space Systems, Chapter 7: Avionics and Flight Management, Chapter 8: Aerospace Reviews, Chapter 9: Supporting Technologies for Aerospace 410 0$aApplied mechanics and materials ;$vv. 629. 606 $aSpace vehicles$vCongresses 608 $aElectronic books. 615 0$aSpace vehicles 676 $a629.1323 702 $aVaratharajoo$b R. 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910459893603321 996 $aAEROTECH V$92145727 997 $aUNINA LEADER 02120nam1 22004573i 450 001 PAL0007302 005 20231121125602.0 020 $aIT$b731720 100 $a20021029g1972 ||||0itac50 ba 101 | $aita 102 $ait 181 1$6z01$ai $bxxxe 182 1$6z01$an 200 1 $aOpere scelte di Giuseppe Baretti$fa cura di Bruno Maier 210 $aTorino$cUnione tipografico-editrice torinese 215 $a v.$d24 cm. 225 | $aClassici italiani$v29 410 0$1001CFI0032661$12001 $aClassici italiani$v29 463 1$1001MIL0203383$12000 $a1$fdi Giuseppe Baretti$v1 463 1$1001MIL0203385$12000 $a2$fdi Giuseppe Baretti$v2 676 $a851.6$9Poesia italiana. 1748-1814$v22 676 $a858.2$9Miscellanea italiana. 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DEI LINCEI E CORSINIANA$bRM0418 899 $aFondazione Marco Besso$bRM0211 899 $aBiblioteca Del Monumento Nazionale Di Montecassino$bFR0084 899 $aBiblioteca umanistica Giorgio Aprea$bFR0017 912 $aPAL0007302 950 1$aBiblioteca umanistica Giorgio Aprea$d 52S.L. 850 UTET Bar.1$d 52S.L. 850 UTET Bar.2 977 $a 01$a 04$a 10$a 14$a 25$a 52 996 $aOpere scelte di Giuseppe Baretti$91673954 997 $aUNICAS