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Precomputed Panel Solver for Aerodynamics Simulation

Published: 23 March 2018 Publication History

Abstract

In this article, we introduce an efficient and versatile numerical aerodynamics model for general three-dimensional geometry shapes in potential flow. The proposed model has low computational cost and achieves an accuracy of moderate fidelity for the aerodynamic loads for a given glider shape. In the geometry preprocessing steps of our model, lifting-wing surfaces are recognized, and wake panels are generated automatically along the trailing edges. The proposed aerodynamics model improves the potential theory-based panel method. Furthermore, a new quadratic expression for aerodynamic forces and moments is proposed. It consists of geometry-dependent aerodynamic coefficient matrices and has a continuous representation for the drag/lift-force coefficients. Our model enables natural and real-time aerodynamics simulations combined with general rigid-body simulators for interactive animation. We also present a design system for original gliders. It uses an assembly-based modeling interface and achieves interactive feedback by leveraging the partwise precomputation enabled by our method. We illustrate that one can easily design various flyable gliders using our system.

Supplementary Material

xie (xie.zip)
Supplemental movie, appendix, image and software files for, Precomputed Panel Solver for Aerodynamics Simulation
MP4 File (tog37-2-a17-xie.mp4)

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Published In

cover image ACM Transactions on Graphics
ACM Transactions on Graphics  Volume 37, Issue 2
April 2018
244 pages
ISSN:0730-0301
EISSN:1557-7368
DOI:10.1145/3191713
Issue’s Table of Contents
Permission to make digital or hard copies of all or part of this work for personal or classroom use is granted without fee provided that copies are not made or distributed for profit or commercial advantage and that copies bear this notice and the full citation on the first page. Copyrights for components of this work owned by others than ACM must be honored. Abstracting with credit is permitted. To copy otherwise, or republish, to post on servers or to redistribute to lists, requires prior specific permission and/or a fee. Request permissions from [email protected]

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Association for Computing Machinery

New York, NY, United States

Publication History

Published: 23 March 2018
Accepted: 01 February 2018
Revised: 01 January 2018
Received: 01 October 2017
Published in TOG Volume 37, Issue 2

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Author Tags

  1. Aerodynamics
  2. aerodynamic coefficient matrix
  3. glider
  4. real-time animation
  5. wake panels

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  • Research-article
  • Research
  • Refereed

Funding Sources

  • JSPS KAKENHI
  • JST CREST
  • Epson International Foundation

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