Varatharajoo / Romli / Ahmad | AEROTECH V: Progressive Aerospace Research | Buch | 978-3-03835-232-7 | sack.de

Buch, Englisch, 541 Seiten, Format (B × H): 170 mm x 240 mm, Gewicht: 1020 g

Varatharajoo / Romli / Ahmad

AEROTECH V: Progressive Aerospace Research

Selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia
Erscheinungsjahr 2014
ISBN: 978-3-03835-232-7
Verlag: Trans Tech Publications

Selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia

Buch, Englisch, 541 Seiten, Format (B × H): 170 mm x 240 mm, Gewicht: 1020 g

ISBN: 978-3-03835-232-7
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
Varatharajoo / Romli / Ahmad AEROTECH V: Progressive Aerospace Research jetzt bestellen!

Weitere Infos & Material


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 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
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


Eds. R. Varatharajoo, F.I. Romli, K.A. Ahmad, D.L. Majid and F. Mustapha


Ihre Fragen, Wünsche oder Anmerkungen
Vorname*
Nachname*
Ihre E-Mail-Adresse*
Kundennr.
Ihre Nachricht*
Lediglich mit * gekennzeichnete Felder sind Pflichtfelder.
Wenn Sie die im Kontaktformular eingegebenen Daten durch Klick auf den nachfolgenden Button übersenden, erklären Sie sich damit einverstanden, dass wir Ihr Angaben für die Beantwortung Ihrer Anfrage verwenden. Selbstverständlich werden Ihre Daten vertraulich behandelt und nicht an Dritte weitergegeben. Sie können der Verwendung Ihrer Daten jederzeit widersprechen. Das Datenhandling bei Sack Fachmedien erklären wir Ihnen in unserer Datenschutzerklärung.