AEROTECH V : progressive aerospace research : selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia / / edited by R. Varatharajoo [and four others] |
Pubbl/distr/stampa | Switzerland : , : TTP, , [2014] |
Descrizione fisica | 1 online resource (525 p.) |
Disciplina | 629.1323 |
Collana | Applied mechanics and materials |
Soggetto topico | Space vehicles |
Soggetto genere / forma | Electronic books. |
ISBN | 3-03826-616-7 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
AEROTECH V: Progressive Aerospace Research; Preface and Editorial Panel; Table of Contents; 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 ModelAn 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 RadomeModal 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 CascadeSpray 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 ApproachReverse 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 |
Record Nr. | UNINA-9910459893603321 |
Switzerland : , : TTP, , [2014] | ||
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Lo trovi qui: Univ. Federico II | ||
|
AEROTECH V : progressive aerospace research : selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia / / edited by R. Varatharajoo [and four others] |
Pubbl/distr/stampa | Switzerland : , : TTP, , [2014] |
Descrizione fisica | 1 online resource (525 p.) |
Disciplina | 629.1323 |
Collana | Applied mechanics and materials |
Soggetto topico | Space vehicles |
ISBN | 3-03826-616-7 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
AEROTECH V: Progressive Aerospace Research; Preface and Editorial Panel; Table of Contents; 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 ModelAn 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 RadomeModal 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 CascadeSpray 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 ApproachReverse 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 |
Record Nr. | UNINA-9910787244503321 |
Switzerland : , : TTP, , [2014] | ||
![]() | ||
Lo trovi qui: Univ. Federico II | ||
|
AEROTECH V : progressive aerospace research : selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia / / edited by R. Varatharajoo [and four others] |
Pubbl/distr/stampa | Switzerland : , : TTP, , [2014] |
Descrizione fisica | 1 online resource (525 p.) |
Disciplina | 629.1323 |
Collana | Applied mechanics and materials |
Soggetto topico | Space vehicles |
ISBN | 3-03826-616-7 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
AEROTECH V: Progressive Aerospace Research; Preface and Editorial Panel; Table of Contents; 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 ModelAn 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 RadomeModal 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 CascadeSpray 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 ApproachReverse 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 |
Record Nr. | UNINA-9910823858303321 |
Switzerland : , : TTP, , [2014] | ||
![]() | ||
Lo trovi qui: Univ. Federico II | ||
|