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 01699oam 2200445 a 450 001 9910702290903321 005 20121015082424.0 035 $a(CKB)5470000002425235 035 $a(OCoLC)696146180 035 $a(EXLCZ)995470000002425235 100 $a20110111d1984 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aCooperative policies among the North, the South, and OPEC$b[electronic resource] $ean optimal control approach /$fby Jaime Marquez, Peter Pauly 210 1$a[Washington, D.C.] :$c[Board of Governors of the Federal Reserve System],$d[1984] 215 $a1 online resource (50 pages) $cillustrations 225 1 $aInternational finance discussion papers ;$vnumber 247 300 $aTitle from title screen (viewed on Oct. 15, 2012). 300 $a"December 1984." 320 $aIncludes bibliographical references (pages 48-50). 517 $aCooperative policies among the North, the South, and OPEC 606 $aDebts, External$zDeveloping countries 606 $aFiscal policy$xMathematical models 606 $aMonetary policy$xMathematical models 615 0$aDebts, External 615 0$aFiscal policy$xMathematical models. 615 0$aMonetary policy$xMathematical models. 700 $aMa?rquez$b Jaime$0250687 701 $aPauly$b Peter H.$f1947-$01400599 712 02$aBoard of Governors of the Federal Reserve System (U.S.) 801 0$bCUS 801 1$bCUS 801 2$bGPO 906 $aBOOK 912 $a9910702290903321 996 $aCooperative policies among the North, the South, and OPEC$93490704 997 $aUNINA