Intro
Contents
About the Editors
Mach Number Effect on Aeroacoustic Characteristics of Compressible Jet Due to Chevron
1 Introduction
2 Experimental Setup and Test Nozzle
3 Experimental Methods
4 Results
4.1 Aerodynamics Results
4.2 Acoustics Results
5 Conclusion
References
Parametric Study of Turbulent Flow Past a Compression-Decompression Ramp
1 Introduction
2 Flowfield in the Vicinity of CDR
3 Solver Validation
4 Grid Independence
5 Simulation Parameters
6 Simulation Results
6.1 Flow Features
6.2 Separated Flow Extents

7 Summary
References
Validation of Numerical Analysis Results for Pusher Configured Turboprop Engine Air Intake
1 Introduction
2 Geometry and Analysis
2.1 Geometry Details
2.2 Mesh Details
2.3 Numerical Details
2.4 Boundary Conditions
3 CFD Results and Validation
3.1 Computational Results
3.2 Instrumentation and Flight Test
3.3 Validation
4 Conclusion
References
Aero-elastic Analysis of High Aspect Ratio UAV Wing-Based on Two-Way Fluid Structure Interaction
1 Introduction
2 Aero-elasticity
3 Fluid-Structure Interaction

3.1 Monolithic Approach
3.2 Partitioned Approach
3.3 Data Mapping
4 Model Generation
4.1 Flat Composite Plate Wing Divergence Study
4.2 Large AR Wing Divergence Study
5 Mesh and Boundary Conditions
5.1 Finite Elements Analysis
5.2 Computational Fluid Dynamics
6 Solver Setup
6.1 Computational Fluid Dynamics (CFD)
6.2 Finite Element Method (FEM)
6.3 System Coupling
6.4 Input Parameters
7 Results and Discussion
7.1 Grid Independence Study
8 Validation
8.1 Flat Composite Plate Wing Divergence Study
8.2 Large AR Wing Divergence Study

9 Conclusion
References
Numerical Study of Effect of Adjacent Blades Oscillation in a Compressor Cascade
1 Introduction
2 Numerical Setup
3 Results and Discussion
3.1 Validation
3.2 Effect of Reduced Frequency
3.3 Effect of Stagnation Point Location on Reattachment Length
4 Conclusions
References
Effect of Incoming Wakes on Losses of a Low-Pressure Turbine of a Gas Turbine Engine
1 Introduction
2 Description of the Problem
3 Computational Methodology
4 Grid Generation
5 Boundary Conditions
6 Computational Time and Convergence

7 Results and Discussion
8 Conclusions
References
Effect of Axial Location on the Performance of a Control Jet in a Supersonic Cross Flow
1 Introduction
2 Methodology
3 Validation and Grid Independence Study
4 Results
4.1 Shock Structures
4.2 Vortex Structures
4.3 Surface Pressure Distribution
4.4 Force and Moment Due to Interaction
4.5 Jet Effectiveness
5 Conclusion
References
Effect of Chord Variation on Subsonic Aerodynamics of Grid Fins
1 Introduction
2 Numerical Methodology
2.1 Geometry
2.2 Mesh and Boundary Conditions