Sonstiges, Englisch, Band Volume 225, 750 Seiten, Format (B × H): 125 mm x 142 mm, Gewicht: 200 g
Sonstiges, Englisch, Band Volume 225, 750 Seiten, Format (B × H): 125 mm x 142 mm, Gewicht: 200 g
Reihe: Applied Mechanics and Materials
ISBN: 978-3-03795-314-3
Verlag: Trans Tech Publications
Volume is indexed by Thomson Reuters CPCI-S (WoS).
This special collection covers aspects of research in aerodynamics, aerospace structures and materials, propulsion, aerospace design, flight performance, system performance, aerospace management and operation, space systems and aerospace reviews.
Autoren/Hrsg.
Weitere Infos & Material
Wake Frequency Analysis of a Plunging Airfoil with Trailing-Edge StripsNumerical Sensitivity Analysis of Axial Flow Fan 3D Aerodynamics under Off Design ConditionsA Study on the Effect of Upstream Square Blockage of a Rotating CylinderGeneric Modeling and Parametric Study of Flapping Wing Micro-Air-VehicleVentilated Brake Disk Air Streamlining Using Curved VaneAn Experimental Investigation on the Effect of Various Swirl Atomizer Orifice Geometries on the Air Core DiameterThe Effect of Canard to the Aerodynamic Behavior of Blended Wing Body AircraftThe Aerodynamics Investigation of Vortex Trap on Helicopter BladeEffects of Blowing Ratio on Multiple Shallow Angle Film Cooling HolesAssessment 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 TunnelsCoupled Analytical-Numerical Procedure to Solve the Double Wedge Spiked Supersonic Intake Flow FieldRotor-Stator Distance Effect onto Axial Fan Performance ImprovementComparative Study of Vortex Generator Orientation on Wing Surface Considering Delta Vortex GeneratorsCavity Effect of Synthetic Jet Actuators Based on Piezoelectric DiaphragmExperimental and Numerical Investigation onto 1250mm Axial FanNumerical Investigation of Flow-Induced Vibration of a Cantilever Beam for a Piezoelectric Energy HarvesterExperimental Study of Free Stream Turbulent Effects on Dynamic Stall of Pitching Airfoil by Using Particle Image VelocimetryThe Effects of Spatial Resolution in Turbulent Boundary Layers with Pressure GradientsEffect of Laser Pulse Fatigue on the Mechanical Characteristics of a CFRP PlateThe Effect of Laser Cutting Parameters on the Aerospace Structure Panel of CFRP Composite MaterialModal Properties of a Cantilevered Laminated Woven Composite Plate as Affected by Stacking Sequence and Fiber Orientation: An Experimental StudyDamage Identification and Classification in CFRP Laminates ? A SEM Based StudyOptimization of the Composite Truncated Cone Structure Layers under Buckling LoadComputational Simulation for Static and Dynamic Load of Rectangular Plate in Elastic Region for Analysis of Impact Resilient StructureBeneficial Patch Repair Effect on Fatigue Crack Growth of Al-Alloy 7050Geometric Non-Linear Analysis of Composite Laminated Plates Using Higher Order Finite Strip ElementFailure Mechanics of Uniformly Compressed Thin-Walled Box-Section StrutsPrediction of Energy Absorption Capability of Curved Panel Structure; For Wing Leading Edge StudyComputational Analysis of a Truss Type FuselageDamage Classification in CFRP Laminates Using Principal Component Analysis (PCA) ApproachMultiple Delaminations Growth in Composite Laminates under Compressive Cyclic Loading in Post-BucklingStructural Analysis of Light Aircraft Wing ComponentsBuckling Analysis of Ring-Stiffened Laminated Composite Cylindrical Shells by Fourier-Expansion Based Differential Quadrature MethodThe Behaviour of Fibre-Metal Laminates under High Velocity Impact Loading with Different Stacking Sequences of Al AlloyComposite Repair of Curved Stiffened Aluminum Panels under Combined Tension and Shear Cyclic LoadingsFatigue Damage Mechanism of Titanium in Inert EnvironmentsEffect of Rotor Tip Gap Variation at the Rear Stages of an Axial Flow CompressorImpact of Operating and Health Conditions on a Helicopter Turbo-Shaft Hot Section Component Using Creep FactorAn Investigation on the Effect of Variable Valve Timing on Piston Engine for Lightweight AircraftPreliminary Development of Electric Motorcycle Engine for Sport Aviation VehiclesInvestigation into the Temperature Impact on O-Ring?s Sealing Performance Using Advanced Stress Relaxation TestThermodynamic Analysis of Flow Field at the End of Combustor SimulatorMathematical Model Development of TMM25-Single Shaft Turbojet EngineA Novel Design of Landing Gear Oleo Strut Damper Using MR Fluid for Aircraft and UAV?sDesign of Optimum Torsionally Flexible PropRotors for Tilt-Body MAVsA Preliminary Study of Baseline Design Architecture Effects on Aircraft Redesign RisksA New Concurrent Engineering ? Multi Criteria Decision Making Technique for Conceptual Design SelectionConceptual Design of Solar Powered Unmanned Arial VehicleDesign and Analysis of UAV FuselageComputer Aided Design, Analysis and Prototype Development of 2-Axis Stabilized Aerial Image CapturingPreliminary Design of Solar Powered Unmanned Aerial VehicleAircraft Dynamically Similar Model Design Using Simulated AnnealingModel Reference Adaptive Control Design for a Ducted Fan Air Vehicle in Vertical PlaneDesign and Test of a Vertical-Axis Wind Turbine with Pitch ControlImplementation of Extreme Low Power Micro-Controller for a Wireless Structural Health Monitoring (SHM) SystemDevelopment of Simple-Structure Magnetic Membrane Actuator for Synthetic Jet ApplicationAutomatic Monitoring of Photovoltaic Cells Performance on Solar AircraftPerformance Analysis of Smart Composite Structure Using Shape Memory Alloy ActuatorsTwo-Step Electroplating Process in Fabrication of Thermal Bimorph Cantilever Actuator for Flow Control ApplicationInvestigation on the Effect of Airspeed and Altitude to Phugoid Mode of a Small Unmanned Blended Wing-Body Aircraft with Canard as a Longitudinal Control SurfaceEmissions Performance Study for Conventional Aircraft DesignsStability Analysis of a Light Aircraft Configuration Using Computational Fluid DynamicsOn the Evaluation of Negative Altitude Requirement for Flutter Speed Boundary of Transport Aircraft and UAVThree Dimensional Path Planning Algorithm for Small UAVs Incorporating Existing Dynamic Soaring HeuristicsInvestigation on a Flexible Tether Slackness Based on In- and Out-of Plane Libration AnglesSpacecraft Attitude and System Identification Using Marginal Reduced UKF Utilizing the Sun and Calibrated TAM SensorsSpray Characteristics of Swirl Effervescent Injector in Rocket Application: A ReviewParametric Study of Ground-Track Based Performance Measure Requirements for the Optimization of Near Earth Twin-Spacecrafts TrajectoryLoad Cell Application in Rocket Thrust Measurement SystemApplication of Airborne LiDAR-Derived Parameters and Probabilistic-Based Frequency Ratio Model in Landslide Susceptibility MappingDiurnal and Seasonal Variation of Critical Frequency in Malaysia from 2005 to 2007S.H.E.E.P. for Sleeping in Zero-GPassive Attitude Control Torque Generation Performances of a Gravity Gradient Stabilized SatelliteComparison between H2 and H8 Optimal Control Solutions for a Combined Energy and Attitude Control SystemSoret Measurement for Multi-Component Hydrocarbon Mixtures from Space Experiment Conducted Onboard FOTON M3 Unmanned SatelliteDesigning and Developing a Ground Operation Software for Picosatellite Operation and Data ProcessingSingle Parameter-Based Neural Networks Prediction of TECRemote Sensing Data Derived Parameters and its Use in Landslide Susceptibility Assessment Using Shannon?s Entropy and GISPreliminary Hardware Design and Development of On-Board Data Handling for Pico-Satellite in National Space AgencyThermal Analysis of CUBESAT in Worse Case Hot and Cold Environment Using FEA MethodApplication of Back Propagation Neural Network Algorithms on Modeling Failure of B-737 Bleed Air System Valves in Desert ConditionsReliability Analysis for the Power and Propulsion System of Stratospheric AirshipA Study of Flight Pad Time for Scheduling ProcessRVSM Implementation in MalaysiaMaintainability Prediction for Aircraft Mechanical Components Utilizing Aircraft Feedback InformationInvestigating Imperfect Inspection of Avionics System and its Relationship with Availability PercentageLoosening Monitoring of Bolted Joints Using Optical Fiber Bending Sensor for Aircraft Lug AssemblyComparative Study on Aircraft Landing Instruments: Accuracies and LimitationsUnmanned Aerial Systems Platform Research PrognosisSuggestions for a Roadmap towards Becoming a Launch Capable NationSubsonic Wind Tunnels in Malaysia: A ReviewShort-Term and Long-Term Feedstock Bio Jet Fuel for Green Environment of Air Transport in Climate Change Awareness
