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Aerodynamic Modeling of an Unmanned Aerial Vehicle Using a Computational Fluid Dynamics Prediction Code

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2009, Master of Science (MS), Ohio University, Electrical Engineering (Engineering and Technology).
The process of creating a six degree-of-freedom model for an aerospace vehicle requires detailed knowledge of the aerodynamic characteristics. This thesis presents an implementation of a Computational Fluid Dynamics (CFD) predictioncomputer code to generate aerodynamic coefficients for the Brumby Mk. I Unmanned Aerial Vehicle (UAV). The aerodynamic coefficients include both the force and moment coefficients. These values are verified by creating a Matlab/Simulink six degree-of-freedom model.
Douglas A. Lawrence, PhD (Advisor)
Jerrel Mitchell, PhD (Committee Member)
Jeffrey Dill, PhD (Committee Member)
William Kaufman, PhD (Committee Member)
192 p.

Recommended Citations

Citations

  • Rose, I. D. (2009). Aerodynamic Modeling of an Unmanned Aerial Vehicle Using a Computational Fluid Dynamics Prediction Code [Master's thesis, Ohio University]. OhioLINK Electronic Theses and Dissertations Center. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1237481460

    APA Style (7th edition)

  • Rose, Isaac. Aerodynamic Modeling of an Unmanned Aerial Vehicle Using a Computational Fluid Dynamics Prediction Code. 2009. Ohio University, Master's thesis. OhioLINK Electronic Theses and Dissertations Center, http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1237481460.

    MLA Style (8th edition)

  • Rose, Isaac. "Aerodynamic Modeling of an Unmanned Aerial Vehicle Using a Computational Fluid Dynamics Prediction Code." Master's thesis, Ohio University, 2009. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1237481460

    Chicago Manual of Style (17th edition)