Phillip J Ansell

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Research Output

2020

Experimental characterization of a novel cyclotronic plasma actuator

Hristov, G. K., Ansell, P. J., Zimmerman, J. W. & Carroll, D. L., Jan 1 2020, In : AIAA journal. 58, 2, p. 747-756 10 p.

Research output: Contribution to journalArticle

Multiscale vortex characteristics of dynamic stall from empirical mode decomposition

Ansell, P. J. & Mulleners, K., Jan 1 2020, In : AIAA journal. 58, 2, p. 600-617 18 p.

Research output: Contribution to journalArticle

Open Access
2019

Characterization of a Griffith-type transonic, laminar-flow airfoil

Collazo Garcia, A. R. & Ansell, P. J., Jan 1 2019, In : Journal of Aircraft. 56, 4, p. 1597-1609 13 p.

Research output: Contribution to journalArticle

Hybrid-electric regional jet aircraft operation efficiency

Wroblewski, G. E. & Ansell, P. J., Jan 1 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 proceedingConference contribution

Influence of aspect ratio on dynamic stall of a finite wing

Angulo, I. A. & Ansell, P. J., Jan 1 2019, In : AIAA journal. 57, 7, p. 2722-2733 12 p.

Research output: Contribution to journalArticle

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

Wroblewski, G. E. & Ansell, P. J., Jan 1 2019, In : Journal of Aircraft. 56, 3, p. 1200-1213 14 p.

Research output: Contribution to journalArticle

Optimal hyperelliptic cambered span configurations for minimum drag

Ranjan, P., Ansell, P. J. & James, K. A., Jan 1 2019, In : Journal of Aircraft. 56, 1, p. 356-368 13 p.

Research output: Contribution to journalArticle

Unsteady flow physics of airfoil dynamic stall

Gupta, R. & Ansell, P. J., Jan 1 2019, In : AIAA journal. 57, 1, p. 165-175 11 p.

Research output: Contribution to journalArticle

2018

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

Perry, A. T., Ansell, P. J. & Kerho, M. F., Nov 1 2018, In : Journal of Aircraft. 55, 6, p. 2414-2426 13 p.

Research output: Contribution to journalArticle

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

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

Closed-loop trailing-edge separation control system using empirical mode decomposition

Gupta, R. & Ansell, P. J., Jan 1 2018, In : AIAA journal. 56, 1, p. 121-131 11 p.

Research output: Contribution to journalArticle

Computational analysis of vortex wakes without near-field rollup characteristics

Ranjan, P. & Ansell, P. J., Jan 1 2018, In : Journal of Aircraft. 55, 5, p. 2008-2021 14 p.

Research output: Contribution to journalArticle

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

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

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

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

Fast and Adaptive Empirical Mode Decomposition for Multidimensional, Multivariate Signals

Thirumalaisamy, M. R. & Ansell, P. J., Oct 2018, In : IEEE Signal Processing Letters. 25, 10, p. 1550-1554 5 p., 8447300.

Research output: Contribution to journalArticle

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

Influence of freestream velocity on tilt-rotor fountain effect

Hong, J. W. & Ansell, P. J., Jan 1 2018, In : Journal of Aircraft. 55, 4, p. 1742-1745 4 p.

Research output: Contribution to journalArticle

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

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

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

Dean, T. S., Wroblewski, G. E. & Ansell, P. J., Nov 1 2018, In : Journal of Aircraft. 55, 6, p. 2454-2465 12 p.

Research output: Contribution to journalArticle

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

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

Poststall hysteresis and flowfield unsteadiness on a NACA 0012 airfoil

Hristov, G. & Ansell, P. J., Jan 1 2018, In : AIAA journal. 56, 7, p. 2528-2539 12 p.

Research output: Contribution to journalArticle

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

Yi, X., Sanchez, R., Haran, K., 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

2017

Crossflow fan power requirements for boundary-layer suction in transonic flow

Perry, A. T. & Ansell, P. J., Jan 1 2017, In : Journal of Aircraft. 54, 3, p. 1216-1219 4 p.

Research output: Contribution to journalArticle

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

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

Prediction and experimental evaluation of planar wing spanloads for minimum drag

Wroblewski, G. E. & Ansell, P. J., Sep 2017, In : Journal of Aircraft. 54, 5, p. 1664-1674 11 p.

Research output: Contribution to journalArticle

Separation of unsteady scales in a mixing layer using empirical mode decomposition

Ansell, P. J. & Balajewicz, M. J., Jan 1 2017, In : AIAA journal. 55, 2, p. 419-434 16 p.

Research output: Contribution to journalArticle

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

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

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

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; vol. 0).

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

Unsteady modes in flowfield about airfoil with horn-ice shape

Ansell, P. J. & Bragg, M. B., Jan 1 2016, In : Journal of Aircraft. 53, 2, p. 475-486 12 p.

Research output: Contribution to journalArticle

2015

Characterization of low-frequency oscillations in the flowfield about an iced airfoil

Ansell, P. J. & Bragg, M. B., Mar 1 2015, In : AIAA journal. 53, 3, p. 629-637 9 p.

Research output: Contribution to journalArticle

2014

Application of a hinge-moment-based envelope protection system on a wing

Ansell, P. J., Kerho, M. F. & Bragg, M. B., Nov 1 2014, In : Journal of Aircraft. 51, 6, p. 2038-2042 5 p.

Research output: Contribution to journalArticle

Measurement of unsteady flow reattachment on an airfoil with an ice shape

Ansell, P. J. & Bragg, M. B., Mar 1 2014, In : AIAA journal. 52, 3, p. 656-659 4 p.

Research output: Contribution to journalComment/debate

Study of burst wakes in a multi-element airfoil flowfield

Pomeroy, B. W., Diebold, J. M., Ansell, P. J. & Selig, M. S., Apr 2014, In : AIAA journal. 52, 4, p. 821-831 11 p.

Research output: Contribution to journalArticle

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

2013

A study of burst wakes in a multielement airfoil flowfield

Pomeroy, B. W., Ansell, P. J., Diebold, J. M. & Selig, M. S., Sep 16 2013.

Research output: Contribution to conferencePaper

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

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

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

2011

Envelope protection system for iced airfoils using flap hinge moment

Ansell, P. J., Bragg, M. B. & Kerho, M. F., Jan 1 2011, In : SAE Technical Papers.

Research output: Contribution to journalConference article

Stall warning using flap hinge moment measurements

Ansell, P. J., Bragg, M. B. & Kerho, M. F., Jan 1 2011, In : Journal of Aircraft. 48, 5, p. 1822-1824 3 p.

Research output: Contribution to journalArticle

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