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1. A Cartesian Immersed Boundary Method Study of Damaged and Undamaged Airfoil Performance

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6. QUALIFICATION OF AIRFOIL TRANSITION MEASUREMENTS TAKEN IN THE PENN STATE LOW-SPEED, LOW-TURBULENCE WIND TUNNEL

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8. An Investigation of the Aerodynamics of Miniature Trailing-Edge Effectors Applied to Rotorcraft

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12. TURBULENCE MEASUREMENTS IN SUPERSONIC JETS WITH OPTICAL DEFLECTOMETRY

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13. Health Monitoring Applications for Small Wind Turbines

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14. COMPUTATIONAL MODELING OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER

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18. INNOVATIVE ENERGY ABSORBING AND LOAD LIMITING DEVICES BASED ON COMPOSITE TUBES

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23. Application of Trade Space Visualization to Discrete and Continuous Complex Dynamical Systems

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24. AEROACOUSTICS OF CONFINED JET-WALL INTERACTIONS WITH APPLICATION TO UNVOICED SPEECH SOUNDS

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30. The Experimental Investigation of a Rotor Icing Model with Shedding

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34. Computer Vision and Target Localization Algorithms for Autonomous Unmanned Aerial Vehicles

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36. Numerical Simulations of Two-Dimensional Laminar Flow Over Bluff Bodies Using the Immersed Boundary Method with Cartesian Grids

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39. PERFORMANCE EVALUATION AND OPTIMIZATION OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER

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41. DEVELOPMENT OF A MODELING CAPABILITY FOR ENERGY HARVESTING MODULES IN ELECTRODYNAMIC TETHER SYSTEMS

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42. Trailing Edge Noise Prediction Using The Nonlinear Disturbance Equations

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43. DESIGN OPTIMIZATION AND DIRECT THRUST MEASUREMENT OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER

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45. BRIDGING METHOD FOR THE JB2006 AND NRLMSISE-00 THERMOSPHERIC DENSITY MODELS IN THE ALTITUDE RANGE OF 140 KM THROUGH 200 KM

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

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52. CELLULAR STRUCTURES WITH INTERNAL FEATURES FOR ENHANCED STRUCTURAL PERFORMANCE

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53. Induced warp systems to obtain Active twist of Rotor Blades

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54. SCALABILITY OF THE FORCE OF A NORMALLY IMPACTING VORTEX RING ON A PLANAR SURFACE

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55. Comparison of interlaminar fracture toughness of filament wound glass/epoxy composites by using MWCNTs or flexible resin

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56. THE DEVELOPMENT AND SYNTHESIS OF MULTIFUNCTIONAL EROSION AND CORROSION RESISTANT TITANIUM-CHROMIUM-NITRIDE COATINGS FOR TURBOMACHINERY APPLICATIONS

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59. Reducing Helicopter Main Rotor Power Requirements Using Multiple Trailing Edge Flaps And Extendable Chord Sections

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60. Shipboard Helicopter Gust Response Alleviation Using Active Trailing Edge Flaps

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61. Investigation of Contact Acoustic Nonlinearities on Metal and Composite Structures via Intensity Based Health Monitoring Systems

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62. Using Numerical Optimization Techniques and General Perturbation Equations to Find Optimal Near-Earth Orbit Transfers

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

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64. Aerodynamic Experiments of a Dual Ducted Fan Vehicle in Hover and Edgewise Flight

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67. PERFORMANCE EVALUATION AND OPTIMIZATION OF HIGH POWER 14.5-GHz MINIATURE MICROWAVE ELECTROTHERMAL THRUSTER

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69. An Adaptive Immersed Boundary Method for CFD Simulation of Multiphase Flows with Moving Internal Bodies

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

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80. Integrated Flight Control Design and Handling Qualities Analysis for a Tiltrotor Aircraft

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84. OPEN-CRACK DAMAGE ASSESSMENTS OF ALUMINUM PANELS USING STRUCTURAL INTENSITY-BASED TECHNIQUES

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85. A Method of Selecting and Configuring Optimal energy Absorbing Cargo Restraint Systems to Improve Crashworthiness

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86. THEORETICAL AND EXPERIMENTAL STUDY OF SCALING METHOD IN THE ROTOR BLADE ICE ACCRETION TEST

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87. COMPARATIVE NUMERICAL ANALYSIS OF FLOW DEVELOPMENT IN THE PRESENCE OF ENDWALL FENCES UPSTREAM OF A VERTICAL CYLINDER IN CROSS FLOW

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88. An Automated Calibration and a Correction Scheme for Total Pressure Gradient Effects of Subminiature Five-Hole Probe

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90. Experimental Method to Measure Pressure-coupled Responses of Induced Solid Rocket Instabilities Using a Next-generation Magnetic Flowmeter

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92. Static and Dynamic Characterization of Composite Materials for Future Driveshaft Systems

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97. Cavitation Assessment and Hydrodynamic Performance Characteristics of a Marine Hydrokinetic Turbine Foil Design

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99. Winglet Design for the Pipistrel Taurus Electro G2 and Twin-taurus G4 with Performance Comparison made Using Flight-path Optimization.

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