Phillip J Ansell

Search results

• 2024

  High-Lift Aerodynamics of Integrated Distributed Propulsion Systems with Thrust Vectoring

  Jois, H., Hong, A. S. & Ansell, P. J., 2024, AIAA SciTech Forum and Exposition, 2024. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA SciTech Forum and Exposition, 2024).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Airfoil Aerodynamics 100%
  • Flow Conditioner 100%
  • Rectangular Nozzle 100%

• Jet-Wake Axial and Swirling Flow Characteristics of Ducted and Unducted Propulsors

  Kopperstad, T. E. & Ansell, P. J., 2024, AIAA SciTech Forum and Exposition, 2024. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA SciTech Forum and Exposition, 2024).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Axial Thrust 100%
  • Momentum Theory 100%
  • Fan Blade 100%
  • Equivalent Actuator 100%
• 2023

  Acoustics of a Rotary Wing with Passive Reduced Tip Vortex in a Static Configuration

  Diaz, M., Yu, D., Ansell, P. & Saxton-Fox, T., 2023, AIAA SciTech Forum and Exposition, 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA SciTech Forum and Exposition, 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Rotors 100%
  • Rotor Disc 50%

• Airfoil Design for Rotors in the Low Reynolds Number Regime

  Patel, Y., Ansell, P. J., Lim, J. W., Barr, S., Weathers, T., Alexandroni, S., Klein, Y., Julius, S. & Abramov, D., 2023, AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Rotors 100%
  • Airfoil 100%
  • Airfoil Optimization 33%
  • Limitations 16%
  • Experimental Result 16%

• Airfoil Performance Sensitivity to Laminar Separation Bubble Characteristics

  Patel, Y. & Ansell, P. J., 2023, AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Bubble Characteristics 100%
  • Infrared Thermography Images 20%
  • Turbulent Reattachment 20%
  • Airfoil Surface 20%

• Air Interactions of Magnetically Driven Plasma Discharges in Crossflow

  Hristov, G. K., Ansell, P. J., Zimmerman, J. W. & Carroll, D. L., 2023, AIAA SciTech Forum and Exposition, 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA SciTech Forum and Exposition, 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Magnetically Driven 100%
  • Cross-flow 100%
  • Plasma Discharge 100%
  • Vortex 100%
  • Boundary Layer 100%

• Analytical Framework for Design of Aero-Propulsive Geometries with Powered Wakes

  Jois, H. & Ansell, P. J., 2023, AIAA SciTech Forum and Exposition, 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA SciTech Forum and Exposition, 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Surface Element 100%
  • Analytical Framework 100%
  • Aviation 50%
  • Flow Visualization 50%
  • Broadening 50%

• Crossflow Interactions of Inclined Fluidic Oscillator Jets

  Awate, V. G. & Ansell, P. J., 2023, AIAA SciTech Forum and Exposition, 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA SciTech Forum and Exposition, 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Fluidics 100%
  • Inclination Angle 100%
  • Vortex 85%
  • Jet Inclination 42%
  • Velocity Field 28%

• Design of Laminar-Flow Airfoils Based On Boundary-Layer Integral Parameters

  Collazo Garcia, A. R. & Ansell, P. J., 2023, AIAA SciTech Forum and Exposition, 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA SciTech Forum and Exposition, 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Boundary Layer 100%
  • Airfoil 100%
  • Integral Parameters 100%
  • Laminar Airfoil 100%
  • Pressure Distribution 50%

• Design of Propellers with Passive Mitigation of Coherent Tip Vortex Roll-up

  Kopperstad, T. E., Borra, A., Beusse, A., Kim, C., Torres De Jesus, E., Saxton-Fox, T. & Ansell, P. J., 2023, AIAA SciTech Forum and Exposition, 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA SciTech Forum and Exposition, 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Bending Moment Coefficient 100%
  • Propeller Design 100%
  • Wake Vorticity 55%

• Electrical Grid Requirements for Sustainable Green Hydrogen Use in Aviation

  Ansell, P. J., 2023, AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Zero-emission Vehicles 100%
  • Liquefied Hydrogen 100%
  • Hydrogen Aircraft 100%
  • Electrolytic Hydrogen 100%
  • Grid Mix 100%

• Hybridization Impact on Emissions for Hydrogen Fuel-Cell/Turbo-Electric Aircraft

  Waddington, E. G., Jois, H., Lauer, M. G., Patel, Y. & Ansell, P. J., 2023, AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Fuel Cell 100%
  • Cell Case 40%
  • Turboshaft 33%
  • Gas Turbine Generator 33%
  • Ducted Propulsor 33%

• Investigating Fluidic Oscillators Embedded in a Slotted-Natural Laminar Flow Airfoil for High-Lift Applications

  Colletti, C. R. & Ansell, P. J., 2023, AIAA SciTech Forum and Exposition, 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA SciTech Forum and Exposition, 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Airfoil 100%
  • Active Flow Control 100%
  • High-lift 100%
  • Natural Laminar Flow Airfoil 100%
  • Fluidic Oscillator 100%

• Multi-fidelity Analysis and Reduced-Order Modeling of Wing-Body Aerodynamics

  Mahesh, K., Shah, A. & Ansell, P. J., 2023, AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Aerodynamics 100%
  • Reduced Order Modeling 100%
  • Centerbody 100%
  • Wing-body 100%
  • Multi-fidelity Analysis 100%

• Preliminary Design and Optimization of a Hydrogen-Electric Aircraft Concept

  Ranjan, P., Das, G. K., Lauer, M. G., Waddington, E. G., Ansell, P. J. & James, K., 2023, AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Preliminary Design 100%
  • Computational Fluid Dynamics 50%
  • Liquid Hydrogen 50%
  • Hydrogen Fuel 50%
  • Drag Reduction 50%

• Steady versus Unsteady Pneumatic Flow Control and Aspects of Practical Integration

  Shmilovich, A., Khodadoust, A., Colletti, C. R. & Ansell, P. J., 2023, AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Pneumatic Flow 100%
  • Oscillator 100%

• Trade-Space Assessment of Liquid Hydrogen Propulsion Systems for Electrified Aircraft

  White, A. S., Waddington, E., Greitzer, E. M., Merret, J. M., Ansell, P. J. & Hall, D. K., 2023, AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Hydrogen Propulsion 100%
  • High Temperature PEM Fuel Cell 25%
  • Modular Optimization 25%
  • Civil Aircraft 25%
• 2022

  Aerodynamic Shape Optimization of a Transonic, Propulsion-Airframe-Integrated Airfoil System

  Lauer, M. G. & Ansell, P. J., 2022, AIAA AVIATION 2022 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2022-3662. (AIAA AVIATION 2022 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Propulsion 100%
  • Airframe 100%
  • Transonic 100%
  • Airfoil 100%
  • Aerodynamic Optimization 100%

• Airfoil Design Framework for Optimized Boundary-Layer Parameters

  Garcia, A. R. C. & Ansell, P. J., 2022, AIAA AVIATION 2022 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA AVIATION 2022 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Design Framework 100%
  • Pressure Distribution 100%
  • Airfoil 100%
  • Airfoil Design 100%
  • Boundary Layer Parameters 100%

• A Parametrization Framework for Multi-Element Airfoil Systems Using Bézier Curves

  Lauer, M. G. & Ansell, P. J., 2022, AIAA AVIATION 2022 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2022-3525. (AIAA AVIATION 2022 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Parametrization 100%
  • Bzier Curves 100%
  • Airfoil 100%
  • Multi-element Airfoil 100%
  • Element Airfoil 100%

• Design and analysis of phononic material for passive flow control

  Park, S., Hristov, G. K., Balasubramanian, S., Goza, A. J., Ansell, P. J. & Matlack, K. H., 2022, AIAA AVIATION 2022 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2022-3330. (AIAA AVIATION 2022 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Passive Flow Control 100%
  • Phononic Materials 100%
  • Control Flow 100%
  • Phononic Material 100%
  • Flow Instability 36%

• Design of Rotary Wings with Passive Mitigation of Coherent Tip Vortex Roll-Up

  Yu, D. & Ansell, P., 2022, AIAA SciTech Forum 2022. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2022-1677. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Rotor 100%
  • Vortex Roll-up 100%
  • Passive Mitigation 100%
  • Rotary Wing 100%
  • Vortex 100%

• Lifting Line Framework for Optimization of Rotary Wing Systems

  Patel, Y. & Ansell, P. J., 2022, AIAA SciTech Forum 2022. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2022-1540. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Rotary Wing 100%
  • Lifting Line 100%
  • Rotors 75%
  • Rotor 50%
  • Induced Velocity 50%

• Plasma-Assisted Burner Array Development using Cyclotronic Arc-Plasma Actuators

  Zimmerman, J. W., Carroll, D. L., Hristov, G. K. & Ansell, P. J., 2022, AIAA SciTech Forum 2022. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2022-2257. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Plasma-assisted 100%
  • Plasma Excitation 100%
  • Plasma Actuator 100%
  • Flame Zone 100%
  • Arc Plasma 100%

• Swirl Characterization of a Cyclotronic Arc Plasma Actuated Axial Air Jet

  Hristov, G. K., Ansell, P. J., Zimmerman, J. W. & Carroll, D. L., 2022, AIAA SciTech Forum 2022. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2022-1548. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Fluid Dynamics 100%
  • Fluidics 100%
  • Vorticity 100%
  • Cross Section 100%
  • Two Dimensional 100%

• System-level utilization of low-grade, mw-scale thermal loads for electric aircraft

  White, A. S., Waddington, E., Merret, J. M., Ansell, P. J., Greitzer, E. M. & Hall, D. K., 2022, AIAA AVIATION 2022 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2022-3291. (AIAA AVIATION 2022 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • System Level 100%
  • Thermal Load 100%
  • Electric Aircraft 100%
  • Fuel Cell 100%
  • Thermal System 100%
• 2021

  Aero-propulsive integration effects of an overwing distributed electric propulsion system

  Yu, D., Ansell, P. & Hristov, G., 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-15 15 p. (AIAA Scitech 2021 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Electric Propulsion System 100%
  • Tip Speed Ratio 100%
  • Integration Effect 100%
  • Aero 100%
  • Distributed Electric Propulsion 100%

• Design of an airfoil morphing leading edge for high-lift applications using a genetic algorithm

  Colletti, C. R. & Ansell, P. J., 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-16 16 p. (AIAA Scitech 2021 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Genetic Algorithm 100%
  • Airfoil 100%
  • High-lift 100%
  • Morphing Leading Edge 100%
  • Leading Edge 100%

• Design of assisted transonic pressure recovery using passive flow control for airfoil geometries

  Collazo Garcia, A. R. & Ansell, P. J., 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-20 20 p. (AIAA Scitech 2021 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Pressure Recovery 100%
  • Transonic 100%
  • Passive Flow Control 100%
  • Airfoil Geometry 100%
  • Control Flow 100%

• Impact of LH₂ Fuel Cell-Electric Propulsion on Aircraft Configuration and Integration

  Waddington, E. G., Merret, J. M. & Ansell, P. J., 2021, AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2021-2409. (AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Fuel Cell 100%
  • Liquid Hydrogen 100%
  • Fuel Cell System 100%
  • Hydrogen Fuel 100%
  • Aircraft Configuration 100%

• Modal analysis of the transonic shock process over a griffith-type, laminar-flow airfoil

  Garcia, A. R. C., Saxton-Fox, T. & Ansell, P. J., 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-16 16 p. (AIAA Scitech 2021 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Modal Analysis 100%
  • Suction 100%
  • Griffith 100%
  • Laminar Airfoil 100%
  • Shock Process 100%

• Multi-Domain Modeling for High Temperature Superconducting Components for the CHEETA Hybrid Propulsion Power System

  Podlaski, M., Khare, A., Vanfretti, L., Sumption, M. & Ansell, P., 2021, AIAA Propulsion and Energy Forum, 2021. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2021-3302. (AIAA Propulsion and Energy Forum, 2021).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • High-temperature Superconductivity 100%
  • High Efficiency 100%
  • Power System 100%
  • Multi-domain Simulation 100%
  • Propulsion Power 100%

• Multi-Domain Modeling for High Temperature Superconducting Components for the CHEETA Hybrid Propulsion Power System

  Podlaski, M., Khare, A., Vanfretti, L., Sumption, M. & Ansell, P., 2021, 2021 AIAA/IEEE Electric Aircraft Technologies Symposium, EATS 2021. Institute of Electrical and Electronics Engineers Inc., (2021 AIAA/IEEE Electric Aircraft Technologies Symposium, EATS 2021).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • High-temperature Superconductivity 100%
  • High Efficiency 100%
  • Power System 100%
  • Multi-domain Simulation 100%
  • Propulsion Power 100%
• 2020

  A bréguet range equation for hybrid-electric jet aircraft sizing and analysis

  Wroblewski, G. E. & Ansell, P. J., Aug 26 2020, AIAA Propulsion and Energy 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-24 24 p. 9235153. (2020 AIAA/IEEE Electric Aircraft Technologies Symposium, EATS 2020).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Hybrid Electric 100%
  • Range Equation 100%
  • Jet Aircraft 100%
  • Aircraft Sizing 100%
  • Mach Number 100%

• Characterization of inclined oscillating jet and crossflow interaction for use in active flow control

  Awate, V. G. & Ansell, P. J., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2020 Forum; vol. 1 PartF).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Active Flow Control 100%
  • Fluidic Oscillator 100%
  • Oscillating Jet 100%
  • Oscillating Crossflow 100%
  • Fluidics 100%

• Experimental characterization of a novel cyclotronic plasma actuator

  Hristov, G. K., Ansell, P. J., Zimmerman, J. W. & Carroll, D. L., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2020 Forum; vol. 1 PartF).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Vorticity 100%
  • Current-Voltage Characteristic 100%
  • Experimental Characterization 100%
  • Power Level 100%
  • Actuator 100%

• Initial Steps in Modeling of CHEETA Hybrid Propulsion Aircraft Vehicle Power Systems using Modelica

  Podlaski, M., Vanfretti, L., Khare, A., Nademi, H., Ansell, P., Haran, K. & Balachandran, T., Aug 26 2020, 2020 AIAA/IEEE Electric Aircraft Technologies Symposium, EATS 2020. Institute of Electrical and Electronics Engineers Inc., 9235182. (2020 AIAA/IEEE Electric Aircraft Technologies Symposium, EATS 2020).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Vehicle Power Systems 100%
  • Different Power Systems 100%
  • Eciency 100%
  • Power System Configuration 100%
  • Electrified Propulsion 100%
• 2019

  Circuit studies for cyclotronic plasma actuators

  Zimmerman, J. W., Carroll, D. L., Hristov, G. K., Vahora, M. & Ansell, P. J., 2019, AIAA Aviation 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-16 16 p. (AIAA Aviation 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Plasma Arc 100%
  • Plasma Actuator 100%
  • Arc Plasma 100%
  • Plasma Jet 100%
  • Magnetic Field 40%

• Development and validation of a continuous, open-return transonic wind tunnel

  Collazo Garcia, A. R. & Ansell, P. J., 2019, AIAA Aviation 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aviation 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Aspect Ratio 100%
  • Turbulence Intensity 100%
  • Porous Wall 100%
  • Transonic Wind Tunnel 100%
  • Flow Angularity 100%

• Effect of geometric parameters and flow conditions on the frequency of fluidic oscillators for active flow control

  Colletti, C. R., Awate, V. G. & Ansell, P. J., 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Flow Condition 100%
  • Parameter Condition 100%
  • Geometric Parameters 100%
  • Active Flow Control 100%
  • Geometric Flow 100%

• Flight trajectory optimization of a sailplane after rope break during an aerotow takeoff

  Collazo Garcia, A. R., Ranjan, P., James, K. A. & Ansell, P. J., 2019, AIAA Aviation 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aviation 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Take-off 100%
  • Rope 100%
  • Sailplane 100%
  • Flight Trajectory Optimization 100%
  • Flight Trajectory 100%

• High-lift configuration of a slotted natural laminar flow airfoil

  Twiss, D. C., Colletti, C. R. & Ansell, P. J., 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  Open Access

  • Rigging 100%
  • High-lift 100%
  • Natural Laminar Flow Airfoil 100%
  • Laminar Flows 100%
  • Airfoil 100%

• Hybrid-electric regional jet aircraft operation efficiency

  Wroblewski, G. E. & Ansell, P. J., 2019, AIAA Propulsion and Energy Forum and Exposition, 2019. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Propulsion and Energy Forum and Exposition, 2019).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Hybrid Electric 100%
  • Operational Efficiency 100%
  • Aircraft Operation 100%
  • Jet Aircraft 100%
  • Regional Jet 100%

• Scaling studies of cyclotronic plasma actuators for active flow control applications

  Zimmerman, J. W., Carroll, D. L., Hristov, G. K., Vahora, M., Motz, M. K., Richardson, D. R. & Ansell, P. J., 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Actuator 100%
  • Control Applications 100%
  • Plasma Actuator 100%
  • Active Flow Control 100%
  • Arc Plasma 100%

• System identification and dynamics modeling of a distributed electric propulsion aircraft

  Perry, A. T., Bretl, T. & Ansell, P. J., 2019, AIAA Aviation 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-14 14 p. (AIAA Aviation 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • System Dynamics Model 100%
  • System Identification 100%
  • Distributed Electric Propulsion Aircraft 100%
  • Electric Propulsion 100%
  • Flight Test 100%
• 2018

  Aero-propulsive and propulsor cross-coupling effects on a distributed propulsion system

  Perry, A. T., Ansell, P. J. & Kerho, M. F., 2018, AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Airfoil 100%
  • Aero 100%
  • Propulsor 100%
  • Distributed Propulsion System 100%
  • Cross-coupling Effect 100%

• A Review of Distributed Electric Propulsion Concepts for Air Vehicle Technology

  Kim, H. D., Perry, A. T. & Ansell, P. J., Nov 29 2018, 2018 AIAA/IEEE Electric Aircraft Technologies Symposium, EATS 2018. Institute of Electrical and Electronics Engineers Inc., 8552794. (2018 AIAA/IEEE Electric Aircraft Technologies Symposium, EATS 2018).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  Open Access

  • Air Vehicle 100%
  • Vehicle Technology 100%
  • Propulsor 100%
  • Distributed Electric Propulsion 100%
  • Electric Propulsion 100%

• Configuration studies for a plasma actuator technique using arc breakdown in a magnetic field

  Zimmerman, J. W., Hristov, G. K., Vahora, M., Ansell, P. J. & Carroll, D. L., 2018, 2018 Flow Control Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3758. (2018 Flow Control Conference).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Magnetic Field 100%
  • Plasma Actuator 100%
  • Arc Breakdown 100%
  • Configuration Study 100%
  • Arc Plasma 100%

• Design and Development of a Dynamically, Scaled Distributed Electric Propulsion Aircraft Testbed

  Pieper, K., Perry, A., Ansell, P. & Bretl, T., Nov 29 2018, 2018 AIAA/IEEE Electric Aircraft Technologies Symposium, EATS 2018. Institute of Electrical and Electronics Engineers Inc., 8552755. (2018 AIAA/IEEE Electric Aircraft Technologies Symposium, EATS 2018).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Propulsion 100%
  • Cirrus 100%
  • Distributed Electric Propulsion Aircraft 100%
  • Distributed Electric Propulsion 100%
  • Electric Ducted Fan 100%

• Development of a plasma actuator with arc breakdown in a magnetic field

  Zimmerman, J. W., Hristov, G. K., Ansell, P. J. & Carroll, D. L., 2018, AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Magnetic Field 100%
  • Plasma Arc 100%
  • Plasma Actuator 100%
  • Arc Breakdown 100%
  • Arc Plasma 100%