Buch, Englisch, 750 Seiten, Format (B × H): 170 mm x 240 mm, Gewicht: 1500 g
Buch, Englisch, 750 Seiten, Format (B × H): 170 mm x 240 mm, Gewicht: 1500 g
ISBN: 978-3-03785-506-5
Verlag: Trans Tech Publications
Autoren/Hrsg.
Weitere Infos & Material
Preface, Editorial, Organizing and Sponsors
Chapter 1: Aerodynamics
Wake Frequency Analysis of a Plunging Airfoil with Trailing-Edge Strips
Numerical Sensitivity Analysis of Axial Flow Fan 3D Aerodynamics under Off Design Conditions
A Study on the Effect of Upstream Square Blockage of a Rotating Cylinder
Generic Modeling and Parametric Study of Flapping Wing Micro-Air-Vehicle
Ventilated Brake Disk Air Streamlining Using Curved Vane
An Experimental Investigation on the Effect of Various Swirl Atomizer Orifice Geometries on the Air Core Diameter
The Effect of Canard to the Aerodynamic Behavior of Blended Wing Body Aircraft
The Aerodynamics Investigation of Vortex Trap on Helicopter Blade
Effects of Blowing Ratio on Multiple Shallow Angle Film Cooling Holes
Assessment on Effects of Under-Relaxation Factors on 2D Incompressible Laminar Flow over a Backward-Facing Step (BFS)
Aerodynamic Interference Correction Methods Case: Subsonic Closed Wind Tunnels
Coupled Analytical-Numerical Procedure to Solve the Double Wedge Spiked Supersonic Intake Flow Field
Rotor-Stator Distance Effect onto Axial Fan Performance Improvement
Comparative Study of Vortex Generator Orientation on Wing Surface Considering Delta Vortex Generators
Cavity Effect of Synthetic Jet Actuators Based on Piezoelectric Diaphragm
Experimental and Numerical Investigation onto 1250mm Axial Fan
Numerical Investigation of Flow-Induced Vibration of a Cantilever Beam for a Piezoelectric Energy Harvester
Experimental Study of Free Stream Turbulent Effects on Dynamic Stall of Pitching Airfoil by Using Particle Image Velocimetry
The Effects of Spatial Resolution in Turbulent Boundary Layers with Pressure Gradients
Chapter 2: Aerospace Structures and Material
Effect of Laser Pulse Fatigue on the Mechanical Characteristics of a CFRP Plate
The Effect of Laser Cutting Parameters on the Aerospace Structure Panel of CFRP Composite Material
Modal Properties of a Cantilevered Laminated Woven Composite Plate as Affected by Stacking Sequence and Fiber Orientation: An Experimental Study
Damage Identification and Classification in CFRP Laminates – A SEM Based Study
Optimization of the Composite Truncated Cone Structure Layers under Buckling Load
Computational Simulation for Static and Dynamic Load of Rectangular Plate in Elastic Region for Analysis of Impact Resilient Structure
Beneficial Patch Repair Effect on Fatigue Crack Growth of Al-Alloy 7050
Geometric Non-Linear Analysis of Composite Laminated Plates Using Higher Order Finite Strip Element
Failure Mechanics of Uniformly Compressed Thin-Walled Box-Section Struts
Prediction of Energy Absorption Capability of Curved Panel Structure; For Wing Leading Edge Study
Computational Analysis of a Truss Type Fuselage
Damage Classification in CFRP Laminates Using Principal Component Analysis (PCA) Approach
Multiple Delaminations Growth in Composite Laminates under Compressive Cyclic Loading in Post-Buckling
Structural Analysis of Light Aircraft Wing Components
Buckling Analysis of Ring-Stiffened Laminated Composite Cylindrical Shells by Fourier-Expansion Based Differential Quadrature Method
The Behaviour of Fibre-Metal Laminates under High Velocity Impact Loading with Different Stacking Sequences of Al Alloy
Composite Repair of Curved Stiffened Aluminum Panels under Combined Tension and Shear Cyclic Loadings
Fatigue Damage Mechanism of Titanium in Inert Environments
Chapter 3: Propulsion
Effect of Rotor Tip Gap Variation at the Rear Stages of an Axial Flow Compressor
Impact of Operating and Health Conditions on a Helicopter Turbo-Shaft Hot Section Component Using Creep Factor
An Investigation on the Effect of Variable Valve Timing on Piston Engine for Lightweight Aircraft
Preliminary Development of Electric Motorcycle Engine for Sport Aviation Vehicles
Investigation into the Temperature Impact on O-Ring’s Sealing Performance Using Advanced Stress Relaxation Test
Thermodynamic Analysis of Flow Field at the End of Combustor Simulator
Mathematical Model Development of TMM25-Single Shaft Turbojet Engine
Chapter 4: Aerospace Design
A Novel Design of Landing Gear Oleo Strut Damper Using MR Fluid for Aircraft and UAV’s
Design of Optimum Torsionally Flexible PropRotors for Tilt-Body MAVs
A Preliminary Study of Baseline Design Architecture Effects on Aircraft Redesign Risks
A New Concurrent Engineering – Multi Criteria Decision Making Technique for Conceptual Design Selection
Conceptual Design of Solar Powered Unmanned Arial Vehicle
Design and Analysis of UAV Fuselage
Computer Aided Design, Analysis and Prototype Development of 2-Axis Stabilized Aerial Image Capturing
Preliminary Design of Solar Powered Unmanned Aerial Vehicle
Aircraft Dynamically Similar Model Design Using Simulated Annealing
Chapter 5: Aerospace System Performance
Model Reference Adaptive Control Design for a Ducted Fan Air Vehicle in Vertical Plane
Design and Test of a Vertical-Axis Wind Turbine with Pitch Control
Implementation of Extreme Low Power Micro-Controller for a Wireless Structural Health Monitoring (SHM) System
Development of Simple-Structure Magnetic Membrane Actuator for Synthetic Jet Application
Automatic Monitoring of Photovoltaic Cells Performance on Solar Aircraft
Performance Analysis of Smart Composite Structure Using Shape Memory Alloy Actuators
Two-Step Electroplating Process in Fabrication of Thermal Bimorph Cantilever Actuator for Flow Control Application
Chapter 6: Flight Performance
Investigation on the Effect of Airspeed and Altitude to Phugoid Mode of a Small Unmanned Blended Wing-Body Aircraft with Canard as a Longitudinal Control Surface
Emissions Performance Study for Conventional Aircraft Designs
Stability Analysis of a Light Aircraft Configuration Using Computational Fluid Dynamics
On the Evaluation of Negative Altitude Requirement for Flutter Speed Boundary of Transport Aircraft and UAV
Three Dimensional Path Planning Algorithm for Small UAVs Incorporating Existing Dynamic Soaring Heuristics
Chapter 7: Space Systems
Investigation on a Flexible Tether Slackness Based on In- and Out-of Plane Libration Angles
Spacecraft Attitude and System Identification Using Marginal Reduced UKF Utilizing the Sun and Calibrated TAM Sensors
Spray Characteristics of Swirl Effervescent Injector in Rocket Application: A Review
Parametric Study of Ground-Track Based Performance Measure Requirements for the Optimization of Near Earth Twin-Spacecrafts Trajectory
Load Cell Application in Rocket Thrust Measurement System
Application of Airborne LiDAR-Derived Parameters and Probabilistic-Based Frequency Ratio Model in Landslide Susceptibility Mapping
Diurnal and Seasonal Variation of Critical Frequency in Malaysia from 2005 to 2007
S.H.E.E.P. for Sleeping in Zero-G
Passive Attitude Control Torque Generation Performances of a Gravity Gradient Stabilized Satellite
Comparison between H2 and H8 Optimal Control Solutions for a Combined Energy and Attitude Control System
Soret Measurement for Multi-Component Hydrocarbon Mixtures from Space Experiment Conducted Onboard FOTON M3 Unmanned Satellite
Designing and Developing a Ground Operation Software for Picosatellite Operation and Data Processing
Single Parameter-Based Neural Networks Prediction of TEC
Remote Sensing Data Derived Parameters and its Use in Landslide Susceptibility Assessment Using Shannon’s Entropy and GIS
Preliminary Hardware Design and Development of On-Board Data Handling for Pico-Satellite in National Space Agency
Thermal Analysis of CUBESAT in Worse Case Hot and Cold Environment Using FEA Method
Chapter 8: Aerospace Management and Operation
Application of Back Propagation Neural Network Algorithms on Modeling Failure of B-737 Bleed Air System Valves in Desert Conditions
Reliability Analysis for the Power and Propulsion System of Stratospheric Airship
A Study of Flight Pad Time for Scheduling Process
RVSM Implementation in Malaysia
Maintainability Prediction for Aircraft Mechanical Components Utilizing Aircraft Feedback Information
Investigating Imperfect Inspection of Avionics System and its Relationship with Availability Percentage
Loosening Monitoring of Bolted Joints Using Optical Fiber Bending Sensor for Aircraft Lug Assembly
Chapter 9: Aerospace Reviews
Comparative Study on Aircraft Landing Instruments: Accuracies and Limitations
Unmanned Aerial Systems Platform Research Prognosis
Suggestions for a Roadmap towards Becoming a Launch Capable Nation
Subsonic Wind Tunnels in Malaysia: A Review
Short-Term and Long-Term Feedstock Bio Jet Fuel for Green Environment of Air Transport in Climate Change Awareness
