Phillip J Ansell

20102019
If you made any changes in Pure, your changes will be visible here soon.

Research Output 2010 2019

Filter
Conference contribution
2019

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., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Fluidics
Flow control
Airfoils
Boundary layers
Recovery

High-lift configuration of a slotted natural laminar flow airfoil

Twiss, D. C., Colletti, C. R. & Ansell, P. J., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Laminar flow
Airfoils
MATLAB
Drag

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., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Flow control
Actuators
Plasmas
Demonstrations
Lorentz force
2018

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

Perry, A. T., Ansell, P. J. & Kerho, M. F., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Propulsion
Fans
Airfoils
Pressure distribution
Drag

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 proceedingConference contribution

Electric propulsion
Air
Aircraft
Takeoff
Landing

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., Jan 1 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 proceedingConference contribution

Actuators
Magnetic fields
Plasmas
Vortex flow
Flow control

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 proceedingConference contribution

Electric propulsion
Testbeds
Fans
Aircraft
Propulsion

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

Zimmerman, J. W., Hristov, G. K., Ansell, P. J. & Carroll, D. L., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Actuators
Magnetic fields
Plasmas
Flow control
Vortex flow

Evaluation of a griffith-type transonic laminar flow airfoil

Collazo Garcia, A. R. & Ansell, P. J., Jan 1 2018, 2018 Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3177. (2018 Applied Aerodynamics Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Laminar flow
Airfoils
Mach number
Angle of attack
Flow control

Influence of aspect ratio on dynamic stall of a finite wing

Angulo, I. A. & Ansell, P. J., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Aspect ratio
Vortex flow
Angle of attack
Airfoils
Reynolds number

Investigation of the effects of reynolds number on the unsteady flow physics of airfoil dynamic stall

Gupta, R. & Ansell, P. J., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Unsteady flow
Airfoils
Reynolds number
Physics
Surface measurement

Mission analysis and component-level sensitivity study of hybrid-electric general aviation propulsion systems

Dean, T. S., Wroblewski, G. E. & Ansell, P. J., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Electric motors
Aviation
Propulsion
Aircraft
Electric propulsion

Mission analysis and emissions for conventional and hybrid-electric commercial transport aircraft

Wroblewski, G. E. & Ansell, P. J., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Transport aircraft
Aircraft
Propulsion
Charging (batteries)
Turbofan engines

Mission Analysis and Emissions for Conventional and Hybrid-Electric Regional Jet Aircraft

Wroblewski, G. E. & Ansell, P. J., Nov 29 2018, 2018 AIAA/IEEE Electric Aircraft Technologies Symposium, EATS 2018. Institute of Electrical and Electronics Engineers Inc., 8552750. (2018 AIAA/IEEE Electric Aircraft Technologies Symposium, EATS 2018).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Jet aircraft
Flight dynamics
Aircraft
Transport aircraft
MATLAB

Self-Pumped Air-Cooling Design for a High-Speed High-Specific-Power Motor

Yi, X., Sanchez, R., Haran, K. S., Veres, J., Perry, A. T. & Ansell, P. J., Aug 28 2018, 2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018. Institute of Electrical and Electronics Engineers Inc., p. 1135-1140 6 p. 8450114. (2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

air
Cooling
Fans
fan
Rotors
2017

Plasma actuator with arc breakdown in a magnetic field for active flow control applications

Zimmerman, J. W., Palla, A. D., Carroll, D. L., Hristov, G. K. & Ansell, P. J., Jan 1 2017, 48th AIAA Plasmadynamics and Lasers Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, (48th AIAA Plasmadynamics and Lasers Conference, 2017).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Flow control
Actuators
arcs
breakdown
actuators

Post-stall hysteresis and flow field unsteadiness on an NACA 0012 airfoil

Hristov, G. & Ansell, P. J., Jan 1 2017, AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., AIAA 2017-0997. (AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Airfoils
Hysteresis
Flow fields
Angle of attack
Hysteresis loops

Unsteady flow physics of airfoil dynamic stall

Gupta, R. & Ansell, P. J., Jan 1 2017, AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., AIAA 2017-0999. (AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Unsteady flow
Airfoils
Physics
Vortex flow
Surface measurement
2016

Design, analysis, and evaluation of a propulsive wing concept

Perry, A. T., Ansell, P. J., Kerho, M., Ananda, G. & D’Urso, S., Jan 1 2016, 34th AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, (34th AIAA Applied Aerodynamics Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Airfoils
Fans
Aircraft
Blow molding
Drag

Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil

Gupta, R. & Ansell, P. J., Jan 1 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, (54th AIAA Aerospace Sciences Meeting).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Laminar flow
Airfoils
Sensory feedback
Flow separation
Surface measurement

Prediction and experimental evaluation of planar wing spanloads for minimum drag

Wroblewski, G. E. & Ansell, P. J., Jan 1 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, (54th AIAA Aerospace Sciences Meeting).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Drag
Bending moments
Wind tunnels
Lagrange multipliers
Experiments
2014

Unsteady modes in the flowfield about an airfoil with a horn-ice shape

Ansell, P. J. & Bragg, M. B., Jan 1 2014, 44th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc., (44th AIAA Fluid Dynamics Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Airfoils
Ice
Flow separation
Velocity measurement
Geometry
2013

Characterization of ice-induced low-frequency flowfield oscillations and their effect on airfoil performance

Ansell, P. J. & Bragg, M. B., 2013, 31st AIAA Applied Aerodynamics Conference.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Airfoils
Ice
Wavelet transforms
Wind tunnels

Envelope protection for contaminant-induced adverse aerodynamics on a wing using flap hinge moment measurements

Ansell, P. J., Kerho, M. F. & Bragg, M. B., 2013, 31st AIAA Applied Aerodynamics Conference.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Hinges
Aerodynamics
Impurities
Contamination
Detectors
2012

Measurement of unsteady flow reattachment on an airfoil with a leading-edge horn-ice shape

Ansell, P. J. & Bragg, M. B., Jan 1 2012, 30th AIAA Applied Aerodynamics Conference 2012. American Institute of Aeronautics and Astronautics Inc., p. 611-624 14 p. (30th AIAA Applied Aerodynamics Conference 2012).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Unsteady flow
Airfoils
Ice
Strouhal number
Vortex shedding
2010

Envelope protection system using flap hinge moment measurements

Ansell, P. J., Bragg, M. B. & Kerho, M. F., Jan 1 2010, 28th AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics Inc., 2010-4225. (28th AIAA Applied Aerodynamics Conference; vol. 1).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Hinges
Airfoils
Flight envelopes
Glazes
Angle of attack