Elisa Phillips

ORCID: 0000-0003-3256-8242
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About
Contact & Profiles
Research Areas
  • Plasma and Flow Control in Aerodynamics
  • Fluid Dynamics and Turbulent Flows
  • Aerodynamics and Acoustics in Jet Flows
  • Computational Fluid Dynamics and Aerodynamics
  • Family and Patient Care in Intensive Care Units
  • Aerodynamics and Fluid Dynamics Research
  • Patient-Provider Communication in Healthcare
  • Wind and Air Flow Studies
  • Advanced Aircraft Design and Technologies
  • Communication in Education and Healthcare
  • Otolaryngology and Infectious Diseases
  • Ethics and Legal Issues in Pediatric Healthcare
  • Healthcare Systems and Technology
  • Empathy and Medical Education
  • Child Abuse and Trauma
  • Hematological disorders and diagnostics
  • Aerospace and Aviation Technology
  • Infectious Diseases and Tuberculosis

University of Arizona
2010-2023

Lucile Packard Children's Hospital
2018

Unsteady aerodynamic loads were measured on a NACA 0021 airfoil during rapid flap deflections. Typical dynamic-stall effects like an overshoot in lift, drag, and pitching moment have been observed the absence of active flow control. Final flap-deflection angles rate their deflections varied at constant angle attack. Stall prevention or delay was achieved by fluidic actuators that generated discrete sweeping jets over upper surface deflected simple flap. Static experiments proved...

10.2514/1.j051683 article EN AIAA Journal 2013-02-13

View Video Presentation: https://doi.org/10.2514/6.2023-2310.vid The benefits of Active Flow Control (AFC) become limited when trying to apply it a preexisting geometry that cannot be altered. In order showcase the full potential AFC, and allow technology more prominent in vehicle designs, needs considered during conceptual design phase allowed help shape vehicle's geometry. A current limitation is Computational Fluid Dynamics (CFD) wind tunnel testing are too slow costly rapidly evaluate...

10.2514/6.2023-2310 article EN AIAA SCITECH 2022 Forum 2023-01-19

Unsteady aerodynamic loads on a NACA 0021 airfoil during rapid flap deflections were investigated. Typical dynamic stall effects like an overshoot in lift, drag, and pitching moment have been observed. Flap deflection angle speed varied while the of attack remained constant at = 0 . To prevent accompanying detrimental behavior, fluidic actuators generating discrete sweeping jets integrated into simple airfoil. Initial experiments various angles incidence but proved that these can flow...

10.2514/6.2010-4246 article EN 2010-06-28

A previously healthy 18-year-old girl was evaluated at an urgent care center for a threeday history of sore throat, fever, nausea, vomiting, diarrhea, and myalgias; the diagnosis influenza made that time.Four days later, she presented to our Emergency Department with left sided neck pain swelling, productive cough, worsening dyspnea, pleuritic chest pain.On examination her temperature 36.9 C, heart rate 142 beats per minute, respiratory 18 breaths minute.She had enlarged tonsils without...

10.13175/swjpcc135-17 article EN publisher-specific-oa Southwest Journal of Pulmonary and Critical Care 2017-11-15
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