Jason Howison

ORCID: 0000-0002-1643-5100
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About
Contact & Profiles
Research Areas
  • Computational Fluid Dynamics and Aerodynamics
  • Wind and Air Flow Studies
  • Aerodynamics and Fluid Dynamics Research
  • Fluid Dynamics and Vibration Analysis
  • Particle Dynamics in Fluid Flows
  • Wind Energy Research and Development
  • Planetary Science and Exploration
  • Granular flow and fluidized beds
  • Fluid Dynamics and Turbulent Flows
  • Landslides and related hazards
  • Aerodynamics and Acoustics in Jet Flows
  • Spacecraft and Cryogenic Technologies
  • Higher Education Research Studies
  • Engineering Education and Pedagogy
  • Fluid Dynamics and Mixing
  • Experimental Learning in Engineering
  • Cyclone Separators and Fluid Dynamics
  • Advanced Numerical Methods in Computational Mathematics
  • Heat Transfer and Boiling Studies
  • Fluid Dynamics and Heat Transfer
  • Fluid Dynamics Simulations and Interactions
  • Combustion and flame dynamics
  • Flow Measurement and Analysis
  • Reflective Practices in Education
  • Online and Blended Learning

CFD Research Corporation (United States)
2022-2025

Marshall Space Flight Center
2024

Citadel
2016-2020

North Carolina State University
2020

University of Colorado Colorado Springs
2020

American Society For Engineering Education
2020

Embry–Riddle Aeronautical University
2020

University of Maryland, College Park
2020

Auburn University
2020

University of Tennessee at Knoxville
2013-2017

Abstract An aeroelastic model for wind turbine blades derived from the unsteady Navier‐Stokes equations and a mode shape–based structural dynamics are presented. For turbulent flows, system is closed with Spalart‐Allmaras turbulence model. The computation times aerodynamic solution significantly reduced using harmonic balance method compared to time‐accurate solution. This more robust than standard codes that rely on blade element momentum theory determine forces. Comparisons published...

10.1002/we.2157 article EN Wind Energy 2017-12-06

In this paper, we use the harmonic balance method to study an oscillating S809 airfoil in dynamic stall. The periodic behavior of problem makes it well suited for method, which is able model unsteady aerodynamics at greatly reduced computational costs when compared with time-accurate unsteady-flow solvers. A finite-volume technique based on lower–upper symmetric Gauss–Seidel scheme Roe fluxes used solve Reynolds-averaged Navier–Stokes equations. turbulent viscosity computed one-equation...

10.1002/we.1803 article EN Wind Energy 2014-08-27

10.1016/j.ast.2016.02.037 article EN publisher-specific-oa Aerospace Science and Technology 2016-03-22

The design and performance of two unique fluidized bed particle seeders were assessed experimentally. designed to seed the fuel stream freestream a scramjet combustor for image velocimetry measurements. seeder used alumina powder generate particles has been in past obtain silica is new design. Using probe filter paper, samples collected from output each at operating conditions near those encountered studies. imaged using scanning electron microscope qualitative quantitative data about...

10.2514/1.44469 article EN Journal of Propulsion and Power 2010-04-23

10.2514/6.2013-1107 article EN 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013-01-05

Abstract Particle image velocimetry (PIV) has become a mature technology used in research and industry alike to quantify flow properties non-intrusively. Unfortunately, the cost remains too high for students apply method most undergraduate fluids laboratories. Moreover, high-powered pulsed lasers normally utilized PIV systems can be safety risk presence of large groups undergraduates. In this paper, low-cost acquisition analysis system that readily implemented laboratories is presented. A...

10.18260/1-2--29694 article EN 2020-09-10

In order to accurately model particle-particle and gas-particle interactions in two-fluid Eulerian simulations, constitutive models are required for the solid phase. Discrete element (DEM) simulations can be used generate these models, but as particle mixtures increased complexity, there is also a need automate DEM process. this paper, extract dissipation rate stress terms over range of volume fractions using open-source code LIGGGHTS discussed. Automation process quickly databases different...

10.2514/6.2022-2194 article EN AIAA SCITECH 2022 Forum 2022-01-03

Abstract Traditional course delivery, with daily in-class lecture and a textbook for reference, presents number of shortcomings. In traditional lecture, students must transcribe notes from the board, which may take their attention away critical thinking associated trying to understand material. Additionally, tend not use textbooks as instructor intends, but rather choose pattern match examples homework problems, again limits deeper understanding content. Instructor-developed workbooks have...

10.18260/1-2--35458 article EN 2020 ASEE Virtual Annual Conference Content Access Proceedings 2020-09-08

Abstract Effective out-of-class homework assignments are critical to the success of an engineering curriculum. The number and length these play a crucial role in their ability help students comprehend retain recently acquired knowledge. Assignments that too infrequent often put off until right before due date, at which point effort into completion is typically rushed haphazard. Frequent must be proper difficulty, or can get frustrated with large amount time class disproportionately small...

10.18260/1-2--34510 article EN 2020 ASEE Virtual Annual Conference Content Access Proceedings 2020-09-08

Time-accurate aeroelastic simulations were conducted for a flat plate in low speed flow using FUN3D. In order to create an accurate CFD mesh capable of large deformations associated with limit cycle oscillations (LCOs), the was given thicker profile rounded edges. Good agreements obtained between and published experimental data from flutter up 21 m/s. The cause divergence results beyond this point is unknown, but it may be related structural nonlinearity effects. Sensitivities initial...

10.2514/6.2022-0653 article EN AIAA SCITECH 2022 Forum 2022-01-03
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