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Start Over You searched for: Graduate Program Aerospace Engineering Remove constraint Graduate Program: Aerospace Engineering Committee Member Kenneth Steven Brentner Remove constraint Committee Member: Kenneth Steven Brentner

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1. DUCTED FAN INLET/EXIT AND ROTOR TIP FLOW IMPROVEMENTS FOR VERTICAL LIFT SYSTEMS

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3. On the Nonlinearities in the Noise Radiated from High-Speed Model Jets

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4. EXTENDING ACOUSTIC DATA MEASURED WITH SMALL-SCALE SUPERSONIC MODEL JETS TO PRACTICAL AIRCRAFT EXHAUST JETS

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6. A Higher Order Vortex-Lattice Method with a Force-Free Wake

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8. Trailing Edge Noise Prediction Using The Nonlinear Disturbance Equations

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11. On the Characterization of Noise Sources in Supersonic Shock Containing Jets

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12. The Modeling of Homogeneous Condensation in Free-expanding Plumes with the Direct Simulation Monte Carlo Method

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Open Access

13. A NEW APPROACH TO COMPLETE AIRCRAFT LANDING GEAR NOISE PREDICTION

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Open Access

14. Development of a Trailing-Edge Noise Prediction Method using the Non-Linear Disturbance Equations

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Open Access

15. High Order Unstructured Grid Methods For Computational Aeroacoustics

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16. ACOUSTIC PREDICTION OF HEAVY LIFT ROTOR CONFIGURATIONS USING MOMENTUM SOURCE METHOD

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19. Prediction of Acoustic Scattering in the Time Domain and its Applications to Rotorcraft Noise

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20. The Prediction of Broadband Shock-Associated Noise Using Reynolds-Averaged Navier-Stokes Solutions

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21. ENHANCEMENTS AND INVESTIGATION OF CAPABILITIES TO THE LANDING GEAR MODEL AND ACOUSTIC PREDICTION SOFTWARE

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22. IMPROVED CHEMISTRY MODELS FOR DSMC SIMULATIONS OF IONIZED RAREFIED HYPERSONIC FLOWS

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25. The Prediction of Noise and Installation Effects of High-subsonic Dual-stream Jets in Flight

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27. Non-harmonic Root-pitch Individual-blade Control for the Reduction of Blade-vortex Interaction Noise in Rotorcraft

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28. Wind Turbine Design Using A Free-wake Vortex Method With Winglet Application

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31. Computation of Interactional Aerodynamics for Noise Prediction of Heavy Lift Rotorcraft

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32. In-flight Performance Optimization for Rotorcraft with Redundant Controls

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33. Development of a CFD-Compatible Transition Model Based on Linear Stability Theory

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35. Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts

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36. Development Of A Scalable Gas-dynamics Solver With Adaptive Mesh Refinement

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38. Optimization of Active Flap Deployment for Efficient In-plane Rotor Noise Reduction

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Open Access

39. A multi-scale model for geared transmission aero-thermodynamics

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40. Aerodynamics and Thermal Physics of Helicopter Ice Accretion

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41. A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT

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42. Rotorcraft Simulations with Coupled Flight Dynamics, Free Wake, and Acoustics

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43. Incorporating Acoustic Assessment into the Design and Analysis of Rotorcraft

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44. A UNIFIED FLIGHT CONTROL METHODOLOGY FOR A COMPOUND ROTORCRAFT IN FUNDAMENTAL AND AEROBATIC MANEUVERING FLIGHT

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Open Access

45. Computational Investigation of Convective Heat Transfer on Ice-Roughened Aerodynamic Surfaces

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46. SIMULATION OF SUPERSONIC JET NOISE REDUCTION USING FLUID INSERTS FOR LOW BYPASS RATIO TURBOFANS

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47. Rotorcraft noise prediction system validation and analysis for generating noise abatement procedures

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48. Development of an Acoustic Prediction System for Conceptual Design and Analysis of Rotorcraft

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Open Access

49. A Preliminary Investigation of Propeller-Wing Interaction Noise for eVTOL Aircraft

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Open Access