1. Trailing Edge Noise Prediction Using the Non-Linear Disturbance Equations Open Access Author: Jain, Abhishek Title: Trailing Edge Noise Prediction Using the Non-Linear Disturbance Equations Graduate Program: Aerospace Engineering Keywords: CAACFDTrailing EdgeTurbulenceSynthetic Eddy MethodInflow Boundary Conditions File: Download Thesis_AJ_final1.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-AdvisorPhilip John Morris, Thesis Advisor/Co-Advisor
2. Determining Optimum Conditions For Dual Time Stepping Using Convergence Acceleration Techniques in Computational Aeroacoustics Open Access Author: Rout, Vikram Title: Determining Optimum Conditions For Dual Time Stepping Using Convergence Acceleration Techniques in Computational Aeroacoustics Graduate Program: Aerospace Engineering Keywords: DRPDual Time SteppingImplicit Residual SmoothingMultigrid File: Download Thesis_Vikram_Rout_Final.pdf Committee Members: Philip John Morris, Thesis Advisor/Co-Advisor
3. the implementation of a time domain impedance boundary condition Open Access Author: Suo, Qiuling Title: the implementation of a time domain impedance boundary condition Graduate Program: Aerospace Engineering Keywords: time domain impedance boundary conditionabsorbing boundaryporous airfoil File: Download Qiuling_MS.pdf Committee Members: Philip John Morris, Thesis Advisor/Co-Advisor
4. simulations of the flow generated by fluidic inserts for supersonic jet noise reduction based on steady RANS simulations Open Access Author: Kapusta, Matthew Joseph Title: simulations of the flow generated by fluidic inserts for supersonic jet noise reduction based on steady RANS simulations Graduate Program: Aerospace Engineering Keywords: jet noise reductionfluidic insertssupersonic nozzlesupersonic jet flow fieldfluid injection File: Download Kapusta_MS.pdf Committee Members: Philip John Morris, Thesis Advisor/Co-Advisor
