Proceedings of the International Conference on Modern Research in Aerospace Engineering

Name: Proceedings of the International Conference on Modern Research in Aerospace Engineering | MRAE-2016
Brand: Springer
Price: 149.79 EUR
Availability: OnlineOnly

MRAE-2016

Sanjay Singh Pushkar Raj Samir Tambe(Herausgeber*in)

Springer (Verlag)

Erschienen am 9. Februar 2018

XIV, 373 Seiten

E-Book

PDF mit Wasserzeichen-DRM

Systemvoraussetzungen

978-981-10-5849-3 (ISBN)

149,79 €inkl. 7% MwSt.

Systemvoraussetzungen

für PDF mit Wasserzeichen-DRM

E-Book Einzellizenz

Als Download verfügbar

Beschreibung

Weitere Details

Weitere Ausgaben

Personen

Dr. Sanjay Singh completed his B.E (Aero) in 1998 at PEC Chandigarh. He completed his M.Tech (Aerospace) and Ph.D (Aerospace) at the Indian Institute of Technology Kanpur (IIT Kanpur) in 2002 and 2008, respectively. He served as the Project Associate at IIT Kanpur from March-May, 2002 and July-December, 2006. He has been working as an academic since 2007 and he was appointed as the Director of the Aerospace Engineering Department, Amity University, U.P in 2012. He has authored several articles published in journals and conferences. He has worked in the fields of Flight Mechanics, Stability and Control, and Neural Network. He has been a member of the Institution of Engineering and Technology (IET, UK) since 2013 and a life member of the International Association for Continuing Engineering Education (IACEE), USA, since January 2014. Under his leadership the Aerospace Engineering Department at Amity University received accreditation from National Assessment and Accreditation Cou

ncil (NAAC), IET-UK.

Dr. Pushkar Raj received his M.Tech from the Indian Institute of Technology Bombay (IIT Bombay) in 1991 and his doctorate from the National Institute of Technology (NIT) Kurukshetra in 2013. He is a dynamic professional with 33 years of experience of managing scientific research and development projects at the Defence Research and Development Organization (DRDO), focusing on long-term planning, policymaking, organizational restructuring & change management and coordination with other government departments. He has published several research papers at national and international levels. He is a life member of the Computer Society of India and a fellow of the Institution of Electronics and Telecommunication Engineers (IETE)-Delhi. He has advised on matters related to budget allocation, projects, and induction of DRDO products in the armed forces, paramilitary forces, and police organizations. He has been involved in about 200 DRDO projects to analyze

the reasons for cost and program delivery control (PDC) overruns and suggested solutions. He retired from his position of Director-Defense Technology Commission at the DRDO in 2015.

Dr. Samir Tambe received his B.Tech in Aerospace Engineering from the Indian Institute of Technology Bombay (IIT Bombay) in 2002, M.S, Ph.D, and post doctorate fellowship from the Department of Aerospace Engineering and Engineering Mechanics, University of Cincinnati, in 2004, 2010, and 2012, respectively. He has been working as a Research Assistant Professor at the Department of Aerospace Engineering and Engineering Mechanics, College of Engineering and Applied Sciences, University of Cincinnati since May, 2012. He is a senior member of the prestigious American Institute of Aeronautics and Astronautics (AIAA), and a member of the Institute for Liquid Atomization and Spray Systems (ILASS). His work in the fields of propulsion, combustion, and heat transfer has been pioneering.

Inhalt

Intro
Preface
Acknowledgements
Contents
About the Editors
1 Thermal Decomposition and Stabilization Studies of ADN with AN Impurities in the Presence of Catalysts
1 Introduction
2 Experimental Methodology
2.1 Preparation of ADN
2.2 Characterization of ADN
2.3 Sample Preparation
2.4 Instrumentation
3 Results and Discussion
3.1 DSC/TG-DTG of ADN + Cupric (II) Oxide (CuO)
3.2 DSC/TG-DTG of ADN + Ammonium Metavanadate (NH4VO3)
3.3 DSC/TG-DTG of ADN + Copper Chromite (Cu2Cr2O5)
4 Conclusion
Acknowledgements
References
2 Experimental Investigation of Flame Speed of Fuel-Air Mixture for Varying Air/Fuel Ratio
1 Introduction
2 Experimentation
3 Results and Discussion
4 Conclusion
References
3 Medium Scale Jet Engine Design and Design Validation Through Simulation
1 Introduction
2 Methodology
2.1 Design Specifications
2.2 Design Procedure
2.3 Simulation Modelling
3 Results and Discussions
4 Conclusions
5 Future Work
Acknowledgements
References
4 Eco-Friendly Propellant for Hybrid Rocket Motor
1 Introduction of Hybrid Rocket Motor
2 Advantages of Hybrid Rocket Motor
3 Advantages of Paraffin Wax
4 Advantages of Nitrous Oxide
5 Combustion Process
6 Rocket Propulsion Principle
7 Cold Flow Test
8 Static Testing
9 Results and Discussion
9.1 Chamber Pressure Verses Time Comparison
9.2 Thrust Verses Time Comparison
10 Conclusion
Acknowledgements
References
5 Fluidic Thrust Vectoring of Engine Nozzle
1 Introduction
2 Modeling Methodology
2.1 Computational Approach
2.2 Meshing of the Geometry
2.3 Boundary Conditions
3 Performance Analysis
3.1 Deflection Angle Value
3.2 Results
3.3 Thrust Vectoring Efficiency
4 Conclusion
2D-PIV Measurements in a Novel Swirl Burner Under Isothermal Conditions
1 Introduction
2 Burner Description
3 Experimental Set-up
4 Results and Discussion
4.1 Axial Flow Field
4.2 Tangential Flow Field
5 Conclusion
References
Design of 3D Guidance Law for Tactical Missiles
1 Introduction
2 Missile-Target Engagement Model
3 Guidance Law Design
3.1 Guidance Law Design by Feedback Linearization
4 Simulation Results
5 Conclusions
References
8 MATLAB-Based Graphical User Interface Development of RADAR with the Implementation of Noise Under Various Bands
1 Introduction
2 Methodology
2.1 Design and Processing
2.2 RADAR Range Equation
3 Results
4 Conclusions
References
9 Control of UAV Using GSM Technology
1 Introduction
2 Development of the Android Application
3 Android Device Architecture
3.1 Radio Interface Layer
3.2 RIL to Baseband Communication
3.3 Rooting of the Android Device
3.4 Android Debugging Bridge (ADB)
4 GSM Technology
4.1 GSM Modem
4.2 AT Commands
5 GSM Modem and the Flight Controller Communication
6 Conclusion
Acknowledgements
References
10 Orbital Magnetic Interplanetary Launch System (OMILS)
1 Introduction
2 Oberth Effect
3 Equations of Motion of Oberth Effect
4 Rendezvous Mode
5 The Anchoring Concept
6 The Electromagnetic Module
7 Equation for the Magnetic Acceleration and Calculation
8 Conclusions
References
11 Design and Analysis of Two-Axis Seeker Stabilization System
1 Introduction
2 Stabilization System Description
2.1 Position Mode
2.2 Track Mode
2.3 Decoupling and Isolation Factors
2.4 BLDC Servo System
3 Dynamic Mass Unbalance and Kinematic Couplings
4 Multi-body Dynamic and Modeling
5 Simulation and Results
5.1 Frequency Response
5.2 Time Response (Body Rate Variation on Step Response)
6 Conclusion
References
12 UAV Advancement: From Increasing Endurance, Route Re-Plan and Collision Avoidance, to Safe Landing in Critical Conditions
1 Introduction
2 Lithium-Polymer Battery
2.1 Calculation
3 On Path Charging Facility
4 Collision Avoidance System
5 UAV with Autonomous Level 4
6 Failsafe Parachute Landing
6.1 Calculation
7 Conclusion
References
High Angle of Attack Analysis of Cascade Fin in Subsonic Flow
1 Introduction
2 Computational Approach
2.1 Geometry and Flow Parameters
2.2 Solution Methodology
2.3 Computational Mesh and Boundary Conditions
3 Results and Discussions
3.1 Validation of CFD Results
3.2 Comparison of Aerodynamic Coefficients of 3 Planar Member Cascade of Different g/c Versus Flat Plate
3.3 Pressure Contours at Different a (10°, 30°)-Cascade Fin Versus Flat Plate
3.4 Velocity Contours at Different Angles of Attack (10°, 15°, 40°)-Cascade Fin Versus Flat Plate
4 Conclusions
References
14 CFD Investigation of Supersonic Free Jet from a CD Nozzle
1 Introduction
2 Numerical Method
3 Mesh
4 Boundary Conditions
5 Results and Discussion
5.1 Importance of Mesh Height
5.2 Mesh Sensitivity
5.3 Selection of Turbulence Model
6 Conclusion
Acknowledgements
References
15 Study and Design of Golf Ball Like Dimpled Aircraft 2-D Wing and Effects on Aerodynamic Efficiency
1 Introduction
2 Methodology
2.1 Airfoil Selection and Modeling
2.2 Grid Generation
2.3 Model, Boundary Conditions, and Solver Setup
3 Dimple Application
4 Results
5 Conclusions
References
16 Computational Investigation of the Effect of Various Spike Geometries Mounted on Supersonic Vehicles
1 Introduction
2 Literature Review
3 Computation
4 Results and Discussion
5 Conclusion
6 Future Scope
References
17 Effect of Leading-Edge Tubercle on Aerodynamic Performance of NACA 0021 Airfoil
1 Introduction
2 Computational Setup
2.1 Numerical Simulation Scheme
2.2 Grid Generation and Computational Domain
3 Results and Discussion
3.1 Lift and Drag Coefficient Results
3.1.1 Comparison Between 2D and 3D Results of Unmodified NACA 0021
3.1.2 Modified Airfoil (A2W7.5) Simulation Results
3.2 Surface Pressure Coefficient (CP) Results
3.2.1 Comparison Between 2D and 3D Results of Unmodified NACA 0021
3.2.2 Modified Airfoil (A2W7.5) Simulation Results
3.3 Results of Skin Friction Coefficient (Cf) at 20° Angle of Attack
4 Conclusion
Acknowledgements
References
18 Estimation of Aerodynamic Coefficient for a Variable Span Wing and a C-Wing for Application in Personal Air Vehicles (PAV)
1 Introduction
2 Design Methodologies
3 Results and Discussion
3.1 Theoretical Analysis
3.1.1 Prandtl's Lifting Line Theory
3.1.2 Kroo's Method
3.2 Computational Analysis
4 Conclusion
References
19 Evaluation of the Structural Integrity of Full-Scale Wing of Aerial Vehicle
1 Introduction
2 Description of the Aerial Wing Structure
3 Experimental Test Setup and Procedure
4 Instrumentation
5 Results and Discussions
6 Conclusion
Acknowledgements
References
20 Finite Element Analysis of Hyperbolic Paraboloid Composite Shells for Static Analysis Under Uniform Pressure
1 Introduction
2 Mathematical Formulation
2.1 Formulating Static Problem
3 Results and Discussions
3.1 Clamped Hyperbolic Paraboloid with Cross-Ply (0°/90°/0°/90°) Lamination
3.2 Simply Supported Hyperbolic Paraboloid with Cross-Ply (0°/90°/0°/90°) Lamination
3.3 Simply Supported Hyperbolic Paraboloid with Angle-Ply (45°/-45°/45°/-45°) Lamination
3.4 Alternately Simply Supported and Clamped with Cross-Ply (0°/90°/0°/90°) Lamination
3.5 Alternately Simply Supported and Clamped with Angle-Ply (45°/-45°/45°/-45°) Lamination
4 Conclusions
References
21 Behavior of Rectangular Laminated Composite Plate with Central Hole Under Transverse Loading
1 Introduction
2 Mathematical Formulation
3 Results and Discussions
3.1 Comparison of Symmetric (60°/-60°/-60°/60°) and Antisymmetric (60°/-60°/60°/-60°) with Hole
3.2 Comparison of Symmetric (60°/-60°/-60°/60°) and Antisymmetric (60°/-60°/60°/-60°) Without Hole
4 Conclusion
References
Effect of Aspect Ratio Change on Nonlinear Resonance of Rectangular Aircraft Panel
1 Introduction
2 Governing Equations
3 Results and Discussions
4 Conclusions
References
23 Experimental Validation of the Structural Integrity of a CFRP Aircraft Fuselage
1 Introduction
2 Test Loads
3 Experimental Set-up
4 Instrumentation Involved
5 Necessary Precautions for Testing of Composite Section
6 Results and Discussion
7 Conclusion
References
24 Effect of Natural Frequency of Slender Structure on VIV at Higher Reynolds Numbers
1 Introduction
2 Governing Equations of Fluid Domain
2.1 Conservation of Momentum
2.2 Continuity Equation
2.3 RANS Equation
2.4 k-e Model
2.5 Governing Equation of Motion of Structure
3 Computational Domain and Grid Formation
4 Vortex-Induced Vibration of Circular Cylinder
5 Conclusion
References
25 Evaluation of Vibration of a Crankshaft and a Driveshaft Using FEM
1 Introduction
2 Modelling of Crankshaft and Driveshaft
3 Finite Element Analysis
4 Material and Definition
5 Results and Discussion
6 Parametric Studies
6.1 Weight Comparison (W)
6.2 Natural Frequency (?n)
6.3 Deformation (d)
7 Conclusion
References
26 Magnetic Analysis of an Electromagnetic Band Brake (EMBB)
1 Introduction
2 Methodology
2.1 Design and Processing
2.2 Results and Post-Processing
3 Conclusions
References
27 Experimental Evaluation of Circular Cylindrical Shells with Cutouts Under the Combined Effect of Structural and Thermal Loads
1 Introduction
2 Test Article Preparation
3 Test Setup
3.1 Test Fixture
3.2 Power Controllers
3.3 Control System
3.4 Data Acquisition and Control System
3.5 LVDTs
4 Test Procedure
5 Results and Discussion
6 Conclusions
References
28 Weight Reduction of Structural Members for Ground Vehicles by the Introduction of FRP Composite and Its Implications
1 Introduction
2 Consequences of Vehicular Weight Reduction
2.1 Impact on Fuel Consumption
3 Measures for Vehicular Weight Reduction
3.1 Introduction of Alternative Materials
3.1.1 Properties of Alternative Substitution Materials
3.2 Fiber Composites as Alternative Substitution Materials for Automobiles
4 Methodology
5 Results and Discussions
6 Economics of Vehicular Weight Reduction
7 Conclusion
References
29 Optimization of Surface Grinding Process Parameters Through RSM
1 Introduction
2 Experimentations and Methodology
2.1 Surface Roughness Measurements and MRR Calculation
2.2 Response Surface Methodology
2.3 Regression Models
3 Result and Discussion
4 Conclusions
References
30 Evaluating Significance of Green Manufacturing Enablers Using MOORA Method for Indian Manufacturing Sector
1 Introduction
2 Literature Review
3 Enablers of Green Manufacturing
4 Methodology, Results, and Discussion
5 Conclusions
References
31 Military Airworthiness and Certification Procedures: Global Scenario
1 Airworthiness
2 System Safety
2.1 Flight Safety and Airworthiness
3 Certification
4 Military Certification
5 Military Certification Procedures in Different Countries
6 Military Airworthiness in UK
7 Military Airworthiness in USA
7.1 USAF Military Aircraft Certification Procedure
7.1.1 Design-Based Airworthiness Assessment
7.1.2 Non-design-based Airworthiness Assessment
7.2 Commercial Derivative Aircraft (CDA)
8 Military Airworthiness of Australia
9 Military Airworthiness in Russia
10 European Defence Agencies (EDA)
11 Military Airworthiness in India
11.1 Indian Military Certification Procedure
12 Discussion and Conclusion
References
32 Improving Assembly Line Efficiency and Output Using Assembly Line Balancing and Reducing Non-Value-Added Activities
1 Introduction
2 Problem Modeling
3 Results and Discussions
3.1 Proposed Layout
3.2 Proposed Layout
4 Conclusions
References
33 Mechanical Behavior of Laminated Composite Curved Tubes
1 Introduction
2 Formulation
2.1 Displacement Field of Single-Layer Composite Curved Tubes
2.1.1 Governing Equations in Toroidal Coordinates
2.1.2 General Solution for In-Plane Pure Bending
2.2 Displacement Field of Thick Laminated Composite Curved Tubes
2.2.1 Layerwise Theory (LWT)
3 Analytical Solution
4 Results and Discussion
5 Conclusion
Acknowledgements
References
Cruise Missile Mission Planning Using Genetic Algorithm
1 Introduction
2 Problem Formulation
3 Flight Control System and Vehicle Dynamics
3.1 Threat Function and Trajectory Risk
4 Fitness Function and Search Space
5 Simulation Studies
6 Conclusion
References
35 Design of Power Efficient SRAM on FPGA
1 Introduction
2 SRAM Cell
3 IO Standard
3.1 LVTTL
3.2 Mobile-DDR
4 Proposed Architecture of Memory
5 Power Analysis
5.1 Power Consumption at 1.0 GHz Operating Frequency
5.2 Power Consumption at 1.5 GHz Operating Frequency
5.3 Power Consumption at 2 GHz Operating Frequency
5.4 Power Consumption at 2.5 GHz Operating Frequency
5.5 Power Consumption at 3 GHz Operating Frequency
5.6 Power Consumption at 3.5 GHz Operating Frequency
6 Conclusion
7 Future Scopes
References

Systemvoraussetzungen

Als PDF speichern Als Link merken