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Multi-fidelity analysis and reduced-order modeling of wing-body aerodynamics
Mahesh, Karthik
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https://hdl.handle.net/2142/122027
Description
- Title
- Multi-fidelity analysis and reduced-order modeling of wing-body aerodynamics
- Author(s)
- Mahesh, Karthik
- Issue Date
- 2023-12-04
- Director of Research (if dissertation) or Advisor (if thesis)
- Ansell, Phillip J
- Department of Study
- Aerospace Engineering
- Discipline
- Aerospace Engineering
- Degree Granting Institution
- University of Illinois at Urbana-Champaign
- Degree Name
- M.S.
- Degree Level
- Thesis
- Keyword(s)
- Aerodynamics
- Reduced Order Modeling
- Slender Body Theory
- Wing Theory
- Vortex Lattice Methods
- Vortex Panel Methods
- PANAIR
- AVL
- Lifting Line Theory
- Abstract
- The aerodynamic design benefits and configuration integration challenges of blended wing body (BWB) configurations over traditional tube-and-wing (TAW) designs have been thoroughly studied over the years. Research has shown that an intermediate approach, the lifting-center-body (LCB) configuration is optimal for regional and short-haul passenger aircraft, providing a significant aerodynamic benefit while reducing the integration complexity. This thesis aims to characterize the geometry and configuration aerodynamics of LCB aircraft across a range of wing-body blending. A variety of aerodynamic analysis methods are used to characterize the surface pressure and lift distributions and determine the sensitivity of various performance parameters to the degree of blending, and inform configuration design guidelines through these studies for aerodynamic design of LCB aircraft. It is postulated that spanload optimization strategies can provide significant reduction in induced drag for an LCB configuration over tube-and-wing configurations, and understanding the chordwise effects can further play an important role in the performance of these designs.
- Graduation Semester
- 2023-12
- Type of Resource
- Thesis
- Copyright and License Information
- Copyright 2023 Karthik Mahesh
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