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AEROTECH IV : recent advances in aerospace technologies : selected, peer reviewed papers from the AEROTECH IV, November 21-22, 2012, Kuala Lumpur, Malaysia / edited by R. Varatharajoo, E.J. Abdullah, D.L. Majid, F.I. Romli, A.S. Mohd Rafie and K.A. Ahmad.
- Format:
- Book
- Conference/Event
- Conference Name:
- AEROTECH (4th : 2012 : Kuala Lumpur, Malaysia)
- Aerospace Technology Conference & Exposition (4th : 2012 : Kuala Lumpur, Malaysia)
- Series:
- Applied Mechanics and Materials
- Applied mechanics and materials, 1660-9336 ; v. 225
- Applied Mechanics and Materials ; v.225
- Language:
- English
- Subjects (All):
- Astronautics--Technological innovations--Congresses.
- Astronautics.
- Aeronautics--Congresses.
- Aeronautics.
- Physical Description:
- 1 online resource (586 p.)
- Other Title:
- Recent advances in aerospace technologies
- Place of Publication:
- Durnten-Zurich : Trans Tech Publications, [2012]
- Language Note:
- English
- Summary:
- Advances in aerospace technologies have set new standards in the modern world and have become the benchmark for innovations in various fields. 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. Review from Book News Inc.: The bi-annual conference was founded in Malaysia in 2005 as a platform for the regional aerospace communities to gather and share recent developments, but it is now attracting partic
- Contents:
- AEROTECH IV; Preface, Editorial, Organizing and Sponsors; Table of Contents; 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 AircraftThe 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 GeneratorsCavity 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 MaterialEffect 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 StructureBeneficial 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
- Notes:
- Description based upon print version of record.
- Includes bibliographical references and indexes.
- Description based on print version record.
- ISBN:
- 9783038133117
- 3038133116
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