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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. Enhanced propagation modeling of directional aviation noise: A hybrid parabolic equation-fast field program method

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9. Trailing Edge Noise Prediction Using The Nonlinear Disturbance Equations

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

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

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14. Sonic Boom Postprocessing Functions to Simulate Atmospheric Turbulence Effects

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

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

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17. Unsteady Lift of Thick Airfoils in Incompressible Turbulent Flow

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18. High Order Unstructured Grid Methods For Computational Aeroacoustics

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

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

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

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

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

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

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

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

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34. Pneumatic Transport Modeling of Air/Gas Drilling Hydraulics in Horizontal and Deviated Wellbores

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

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

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

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

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

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

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

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45. Aerodynamics and Thermal Physics of Helicopter Ice Accretion

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

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

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

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

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

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51. The Prediction of Vibratory Stresses in Wall-Bounded Jets due to Unsteady Aeroacoustic Loading

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52. The Development of a Fast Method for the Calculation of Noise from Supersonic Jets

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

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

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

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

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57. Noise Prediction of Rotorcraft Acoustics for a Conceptual eVTOL Design and Conventional Helicopters

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58. Time-Varying Rotor Noise Computations and Analysis of Electric Vertical Take-Off and Landing Aircraft

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59. Theoretical and experimental study of the effects of cyclic pitch variations on rotor noise

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61. Helicopter Noise Modeling With Varying Fidelity Prediction Systems

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62. Studies on the acoustic far-field distance of urban air mobility aircraft

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