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AEROTECH V: Progressive Aerospace Research: Progressive Aerospace Research: Selected, Peer Reviewed Papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia(Volume 629 Applied Mechanics and Materials)

AEROTECH V: Progressive Aerospace Research: Progressive Aerospace Research: Selected, Peer Reviewed Papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia(Volume 629 Applied Mechanics and Materials)

          
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About the Book

This is a 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, and, Chapter 9: Supporting Technologies for Aerospace.

Table of Contents:

  • Preface and Editorial Panel
  • 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
  • Comparison of Digital DATCOM and Wind Tunnel Data of a Winged Hybrid Airship’s Generic Model
  • An 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
  • Quasi Static Analysis of a Biocomposite Aircraft Radome
  • Modal 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
  • Aerodynamics Performance of Endwall Film Cooling under the Influence of Purge Flow in High Pressure Turbine Cascade
  • Spray 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 Vehicle
  • Design and Analysis of an Aircraft Composite Hinge Bracket Using Finite Element Approach
  • Reverse 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
  • Effects of Aircraft Tail Configurations on Sensitivity to Yaw Disturbances
  • Experimental Determination of Low-Cost Servomotor Reliability for Small Unmanned Aircraft Applications
  • Synthesis of Optimal Distributed Measurement Systems for Control of an Elastic Object
  • Investigation into Air Interception Guidance Algorithms for Autonomous Aerial Hard Docking of Dissimilar Platforms
  • Comparison of Auxiliary Power Unit (APU) and Ground Power Unit (GPU) with Life Cycle Analysis in Ground Operations: A Case Study for Domestic Flight in Turkey
  • The Future of Aircraft Feedback Information: Maintainability Allocation Methodology
  • The Performance of Mass Properties Measurement for Satellite’s Structural Model
  • Experimental Study on Variable Deflection Control of SMA Actuated Composite Plate
  • Data Filter Performance for Rocket Thrust Measurement System
  • Travel Time and Cost Analysis of PAVE Application in Malaysia
  • Performance Testing of Anechoic Chamber
  • Bistatic LIDAR System for the Characterisation of Aviation-Related Pollutant Column Densities
  • Computational Analysis and Characterization of Cockpit Environmental Control System of a Fighter Aircraft in Humid Environment
  • Quadrotor UAV Indoor Localization Using Embedded Stereo Camera
  • Chapter 6: Space Systems
  • Tether Tension Performance Utilizing Various Materials for a Coplanar and Non-Coplanar Model of a Flexible Tethered Satellite System
  • Three-Axis Attitude Control Performance of a Small Satellite Using Control Moment Gyroscope
  • A Parametric Study of Interplanetary Mission Using Solar Sail
  • Low Inclination Circular Orbits for Remote Sensing Satellites
  • Flight Management System for Unmanned Reusable Space Vehicle Atmospheric and Re-Entry Trajectory Optimisation
  • Sliding Mode Control Techniques for Combined Energy and Attitude Control System
  • Chapter 7: Avionics and Flight Management
  • Towards an Optical Aircraft Navigation System
  • Real-Time Trajectory Optimisation Models for Next Generation Air Traffic Management Systems
  • Stores Separation Simulation Development: A Roadmap to System Realisation via Intelligent Data Management System
  • An Evaluation of Economic Model for Assessing Aviation Environmental Impacts towards Airline Operations
  • Next Generation Flight Management System for Real-Time Trajectory Based Operations
  • Flight Data Monitoring/Tracker System for Search and Rescue Mission
  • A Laser Obstacle Warning and Avoidance System for Unmanned Aircraft Sense-and-Avoid
  • Chapter 8: Aerospace Reviews
  • Structuring Knowledge Management in Aerospace Open Innovation Alliances Using Industrial Service Blueprinting
  • Wing-in-Ground Effect Vehicles Flight Automatic Control Systems Development Problems
  • Basic Geometries of the New Closed Circuit Wind Tunnel of the Universiti Putra Malaysia (UPM)
  • HTHL Space Vehicles: Concepts and Control Problems
  • A Review on the Impact of Aircraft Cabin Air Quality and Cabin Pressure on Human Wellbeing
  • Kenaf Fibre: Its Potential and Review on Bending Fatigue of Hollow Shaft Composites
  • Effective Range of Unmanned Aerial Vehicle (UAV) in the Malaysian Army Tactical Operations
  • Chapter 9: Supporting Technologies for Aerospace
  • Vibration Analysis of a Cantilevered Beam with Spring Loading at the Tip as a Generic Elastic Structure
  • Computational Analysis of the Groove Effect to Reduce the Cavitation in Ball Valves
  • Effect of Short Time Sintering on the Mechanical Properties of Undoped Zirconia Ceramics
  • Study of Wake Profiles of a Simplified Model of High Speed Train Using RANS and LES Turbulent Models
  • Control of Bubble Growth by Using Virtual Chamber Neck in Micro Nozzle Channel
  • Effect of Sintering Temperature on Functionally Graded Nickel/Alumina Plate
  • Simultaneous PIV and Gradient Heat Flux Measurement of a Circular Cylinder in Cross-Flow
  • Skin Friction Coefficient and Boundary Layer Trend on UKM Aster i-Bond
  • Metallographic Investigation on the Effect of Cryogenic Temperature on Steel Weldments
  • Impact Characterisation of Glass Fibre Reinforced Polymer (GFRP) Type C-600 and E-800 Using a Drop Weight Machine
  • Development of a Wind Tunnel DAQ Using LabVIEW Tools
  • Modeling and Simulation of Solar Irradiance and Daylight Duration for a High-Power-Output Solar Module System
  • Use of Direct Active Thermal Imaging Technique for Sub Surface Delamination Detection in Aviation Composites
  • Multi-Objective Optimization Using Box-Behken of Response Surface Methodology for High-Speed Machining of Inconel 718
  • Anti-Aliasing for the Visualization of Wavefield Propagation
  • Modelling High Velocity Impact on Aluminium Alloy 7075-T6 under Axial Pretension
  • Low Velocity Impact on Woven Kenaf Fiber Reinforced Composites
  • Aerodynamic Analysis of the Preliminary Design of SURIAKAR 4 Using CFD
  • Topology Optimization for Robust Damage Localization Using Aggregated FRFs Statistical Criteria


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Product Details
  • ISBN-13: 9783038352327
  • Publisher: Trans Tech Publications Ltd
  • Publisher Imprint: Trans Tech Publications Ltd
  • Depth: 32
  • Language: English
  • Series Title: Volume 629 Applied Mechanics and Materials
  • Sub Title: Progressive Aerospace Research: Selected, Peer Reviewed Papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia
  • Width: 170 mm
  • ISBN-10: 3038352322
  • Publisher Date: 29 Oct 2014
  • Binding: Paperback
  • Height: 240 mm
  • No of Pages: 541
  • Spine Width: 27 mm
  • Weight: 1020 gr


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