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A Qualitative Single-Case Exploring the Impact of a Mentor and Cohort on Students’ Academic and Career Decisions.
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In: Publications (2022)
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Data underlying the publication: "A Computationally Efficient Moving Horizon Estimator for UWB Localization on Small Quadrotors"" ...
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Data underlying the publication: "A Computationally Efficient Moving Horizon Estimator for UWB Localization on Small Quadrotors"" ...
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Motivations of Low-Income Engineering Transfer Students Influencing Choice and Pursuit of Baccalaureate Degree Attainment
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Salgado, Leo. - : eScholarship, University of California, 2020
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A Human Reliability Assessment Approach to Software Feature Elicitation and Valuation: Automation of NASA’s Robotics Mission Design Process ...
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| 6 |
Global Aviation System: Towards Sustainable Development
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In: International Journal of Aviation, Aeronautics, and Aerospace (2019)
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| 7 |
Julia Language Ephemeris and Physical Constants Reader for Solar System Bodies
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In: Undergraduate Research Symposium - Prescott (2018)
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| 11 |
Unmanned Aerial Systems Operational Challenges When Used Between Regions Where English is not Widely Spoken or Understood: Human Factors Communication
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In: Ian McAndrew (2016)
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| 12 |
Digital Storytelling as an Innovative Element in English for Specific Purposes
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| 13 |
Assessing Safety Culture within a Flight Training Organization
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In: Applied Aviation Sciences - Daytona Beach (2013)
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| 14 |
An Analysis of the Effectiveness of Emergency Locator Transmitters to Reduce Response Time and Locate Wreckage in U.S. General Aviation Accidents
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In: PhD Dissertations and Master's Theses (2011)
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| 15 |
Comparison of Overset Grid and Grid Deformation Techniques Applied to 2-Dimensional NACA Airfoils
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In: Aerospace Engineering (2009)
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Abstract:
This paper documents a comparison of overset grid and grid deformation schemes applied to flapped and non-flapped NACA airfoil configurations in order to determine the relative accuracy and computational efficiency of each method. This study is part of a larger effort to use computational fluid dynamics to perform moving control surface calculations. Three different cases, using both overset and deformed grids, are considered, including: a) lift and moment comparison of a quasi-steady, non-flapped 0012 airfoil, b) lift and moment comparison of a dynamically pitching non-flapped 0012 airfoil, and c) lift comparison of a dynamic pitching and oscillating flapped 0012 airfoil. These results are compared to experimental data from various sources. Two flow solvers of common lineage were used for the computations: Cobalt for overset and rigid mesh motion and AVUS for the deformable mesh motion. All of the methods produced nominally similar results. As expected, the rigid mesh technique required the least amount of computational resources, while the deformable mesh technique required the greatest amount of computational resources due to its serial implementation. However, in the end, it is difficult to recommend one method over another as the application of each method may be dependent on the project being solved.
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Keyword:
Aerospace Engineering
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URL: https://digitalcommons.calpoly.edu/aero_fac/48
https://digitalcommons.calpoly.edu/cgi/viewcontent.cgi?article=1047&context=aero_fac
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| 16 |
An Architecture for the Autonomous Generation of Preference-Based Trajectories
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| 17 |
What do You Mean? Finding Answers to Complex Questions
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In: School of Information Studies - Faculty Scholarship (2003)
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