Varatharajoo / Romli / Ahmad | AEROTECH V: Progressive Aerospace Research | Sonstiges | 978-3-03795-928-2 | sack.de

Sonstiges, Englisch, Band Volume 629, 541 Seiten, Format (B × H): 125 mm x 142 mm, Gewicht: 200 g

Reihe: Applied Mechanics and Materials

Varatharajoo / Romli / Ahmad

AEROTECH V: Progressive Aerospace Research


Erscheinungsjahr 2014
ISBN: 978-3-03795-928-2
Verlag: Trans Tech Publications

Sonstiges, Englisch, Band Volume 629, 541 Seiten, Format (B × H): 125 mm x 142 mm, Gewicht: 200 g

Reihe: Applied Mechanics and Materials

ISBN: 978-3-03795-928-2
Verlag: Trans Tech Publications


Collection 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
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Weitere Infos & Material


Numerical Simulation of Noise Radiated from a Blunt Trailing EdgeFurther Development of the Kinematic and Aerodynamic Modeling and Analysis of Flapping Wing Ornithopter from Basic PrinciplesExperimental Study on the Effect of Skin Flexibility on Aerodynamic Performance of Flapping Wings for Micro Air VehiclesVisualization of Flow Field and Wake over Clean and Under-Loaded WingsNACA 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 ApplicationsSensing Unsteady Pressure on MAV Wings: A New Method for Turbulence AlleviationMultiple Crack Interactions in Bi-Material Plates under Mode I Tension LoadingFinite Element Computational Modeling and Simulation Studies of Non-Penetrating Impact Using Fundamental PrinciplesLCO 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 SectionsOn the Dynamic Model of a Functionally Graded Spinning Structural Element of an Aircraft AppendageA Computational and Analytical Study into the Use of Counter-Flow Fluidic Thrust Vectoring Nozzle for Small Gas Turbine EnginesComputational Exploration of a Two-Spool High Bypass Turbofan Engine's Component Deterioration Effects on Engine PerformanceCFD 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 AtomizerComputational Approach in Sizing of Pulsejet EngineApplication of Coanda Jet for Generating Lift of Micro Air Vehicles - Preliminary Design ConsiderationsPerformance Calculations within the Conceptual Design Process of Hand-Launched AircraftConceptual 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 ApplicationsDevelopment of Blimp Platform for Aerial PhotographyAutonomous Aerial Hard Docking of Fixed and Rotary Wing UAVs: Task Assessment and Solution ArchitectureAeroelastic Tailoring of Composite Wing Design Using Bee Colony OptimisationThe Application of Multiple Vibration Neutralizers for Vibration Control in AircraftEffects of Aircraft Tail Configurations on Sensitivity to Yaw DisturbancesExperimental Determination of Low-Cost Servomotor Reliability for Small Unmanned Aircraft ApplicationsSynthesis of Optimal Distributed Measurement Systems for Control of an Elastic ObjectInvestigation into Air Interception Guidance Algorithms for Autonomous Aerial Hard Docking of Dissimilar PlatformsComparison of Auxiliary Power Unit (APU) and Ground Power Unit (GPU) with Life Cycle Analysis in Ground Operations: A Case Study for Domestic Flight in TurkeyThe Future of Aircraft Feedback Information: Maintainability Allocation MethodologyThe Performance of Mass Properties Measurement for Satellite?s Structural ModelExperimental Study on Variable Deflection Control of SMA Actuated Composite PlateData Filter Performance for Rocket Thrust Measurement SystemTravel Time and Cost Analysis of PAVE Application in MalaysiaPerformance Testing of Anechoic ChamberBistatic LIDAR System for the Characterisation of Aviation-Related Pollutant Column DensitiesComputational Analysis and Characterization of Cockpit Environmental Control System of a Fighter Aircraft in Humid EnvironmentQuadrotor UAV Indoor Localization Using Embedded Stereo CameraTether Tension Performance Utilizing Various Materials for a Coplanar and Non-Coplanar Model of a Flexible Tethered Satellite SystemThree-Axis Attitude Control Performance of a Small Satellite Using Control Moment GyroscopeA Parametric Study of Interplanetary Mission Using Solar SailLow Inclination Circular Orbits for Remote Sensing SatellitesFlight Management System for Unmanned Reusable Space Vehicle Atmospheric and Re-Entry Trajectory OptimisationSliding Mode Control Techniques for Combined Energy and Attitude Control SystemTowards an Optical Aircraft Navigation SystemReal-Time Trajectory Optimisation Models for Next Generation Air Traffic Management SystemsStores Separation Simulation Development: A Roadmap to System Realisation via Intelligent Data Management SystemAn Evaluation of Economic Model for Assessing Aviation Environmental Impacts towards Airline OperationsNext Generation Flight Management System for Real-Time Trajectory Based OperationsFlight Data Monitoring/Tracker System for Search and Rescue MissionA Laser Obstacle Warning and Avoidance System for Unmanned Aircraft Sense-and-AvoidStructuring Knowledge Management in Aerospace Open Innovation Alliances Using Industrial Service BlueprintingWing-in-Ground Effect Vehicles Flight Automatic Control Systems Development ProblemsBasic Geometries of the New Closed Circuit Wind Tunnel of the Universiti Putra Malaysia (UPM)HTHL Space Vehicles: Concepts and Control ProblemsA Review on the Impact of Aircraft Cabin Air Quality and Cabin Pressure on Human WellbeingKenaf Fibre: Its Potential and Review on Bending Fatigue of Hollow Shaft CompositesEffective Range of Unmanned Aerial Vehicle (UAV) in the Malaysian Army Tactical OperationsVibration Analysis of a Cantilevered Beam with Spring Loading at the Tip as a Generic Elastic StructureComputational Analysis of the Groove Effect to Reduce the Cavitation in Ball ValvesEffect of Short Time Sintering on the Mechanical Properties of Undoped Zirconia CeramicsStudy of Wake Profiles of a Simplified Model of High Speed Train Using RANS and LES Turbulent ModelsControl of Bubble Growth by Using Virtual Chamber Neck in Micro Nozzle ChannelEffect of Sintering Temperature on Functionally Graded Nickel/Alumina PlateSimultaneous PIV and Gradient Heat Flux Measurement of a Circular Cylinder in Cross-FlowSkin Friction Coefficient and Boundary Layer Trend on UKM Aster i-BondMetallographic Investigation on the Effect of Cryogenic Temperature on Steel WeldmentsImpact Characterisation of Glass Fibre Reinforced Polymer (GFRP) Type C-600 and E-800 Using a Drop Weight MachineDevelopment of a Wind Tunnel DAQ Using LabVIEW ToolsModeling and Simulation of Solar Irradiance and Daylight Duration for a High-Power-Output Solar Module SystemUse of Direct Active Thermal Imaging Technique for Sub Surface Delamination Detection in Aviation CompositesMulti-Objective Optimization Using Box-Behken of Response Surface Methodology for High-Speed Machining of Inconel 718Anti-Aliasing for the Visualization of Wavefield PropagationModelling High Velocity Impact on Aluminium Alloy 7075-T6 under Axial PretensionLow Velocity Impact on Woven Kenaf Fiber Reinforced CompositesAerodynamic Analysis of the Preliminary Design of SURIAKAR 4 Using CFDTopology Optimization for Robust Damage Localization Using Aggregated FRFs Statistical Criteria


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