Table of Contents

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   Book Overview
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   Chapter 1 Sensitivity Study of Stagger Angle on the Aerodynamic Performance of Transonic Axial Flow Compressors
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   Chapter 2 Numerical Simulations on Performance of a Hybrid and a Tandem Rotor
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   Chapter 3 Flow-Field Investigation of an Inter-compressor Duct Under Different Inflows and Their Influence on the Performance of a Low-Pressure Compressor
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   Chapter 4 Effects of Radial Distortion on Low-Speed Tandem Stage Axial Compressor
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   Chapter 5 Design and Analysis of Outlet Air Collector Duct for Axial Compressor Test Rig
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   Chapter 6 Aerodynamic Design of Axial Flow Turbine for a Small Gas Turbine Engine
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   Chapter 7 Effect of Hub Clearance on Performance of Radial Turbine
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   Chapter 8 Effect of Various Periodic Surface Concepts for Numerical Investigation of Flow Field Through Variable Area LP Turbine Nozzle
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    Chapter 9 Numerical Investigation of Aerodynamic Performance Parameters in Linear Blade Cascade for High-pressure Turbine
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    Chapter 10 Aerodynamic Design of a Axial Turbine Stage for a Small Gas Turbine Engine
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    Chapter 11 Development of Test Bench for Micro Gas Turbine Engine
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    Chapter 12 Development Strategy for Evaluating Gas Turbine Driven High-speed Alternator
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    Chapter 13 Independent Verification and Validation of Aero Engine Propulsion System Software
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    Chapter 14 Influence of Chiral Lattice on Modal Characteristics of Structures
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    Chapter 15 Micromechanics Approach to Determine Fatigue Life of Ceramic Matrix Composite
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    Chapter 16 Design and Analysis of KIIT Nanosatellite’s Micro-Pulsed Plasma Thruster
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    Chapter 17 Use of N 2 O–O 2 as the Oxidizer for the Hybrid Rocket Application
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    Chapter 18 Effect of Protrusion Configuration on Combustion Stability of Hybrid Rocket Motor
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    Chapter 19 Prediction of Wake Structure Transition for a Linear Plug Nozzle Using Detached Eddy Simulation (DES)
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    Chapter 20 Computational Study of Aero-acoustic Feedback in Supersonic Cavity Flow
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    Chapter 21 Numerical Investigation of Blockage of Scramjet Strut Injector Model in a Supersonic Wind Tunnel
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    Chapter 22 Performance Investigation of a Rectangular Ramjet Intake with Throat Flush Slot Bleed System
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    Chapter 23 JP-10 Propellant Powered Rotating Detonation Waves for Enhancing the Performance of Hypersonic and Supersonic Missiles
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    Chapter 24 Design and Analysis of Rotating Detonation Wave Engine
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    Chapter 25 Design and Performance Evaluation of Plug Nozzle for Rotating Detonation Wave Engine
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    Chapter 26 Feasibility Study of Hybrid Propulsion for Light Aircraft
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    Chapter 27 Combustion Synthesis of Functional Nanoparticles
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    Chapter 28 Using Ozone and Hydrogen Peroxide for Manipulating the Velocity Deficits, Detonabilility, and Flammability Limits of Gaseous Detonations
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    Chapter 29 Thermal Design of Cooling Configurations for an Afterburner V-Gutter of Advanced Aeroengine
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    Chapter 30 A Numerical Investigation on the Effect of Lip Geometry with Tangential Film Cooling on an Annular Combustor
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    Chapter 31 Nanoboron Slurry Fuel Droplet Combustion for High-Particle Loading Ratio
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    Chapter 32 Effect of Surface Temperature on Fuel Drop Splashing on Solid Surfaces
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    Chapter 33 Transition Dynamics Between Luminous and Blue Whirling Flames
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    Chapter 34 Flow Dynamics in a Triple Swirl Burner
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    Chapter 35 Sheet Atomization of Gel Propellant Simulant
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    Chapter 36 A Parametric Study on Rotary Slinger Spray Characteristics Using Laser Diagnostics
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    Chapter 37 CFD Analysis of Primary Air Flow Field of a Swirl Injector Using Embedded LES-Based Hybrid Model