Application of MACSYMA and sparse matrix technology to multielement airfoil calculations-Reference-Cited by-同舟云学术

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Application of MACSYMA and sparse matrix technology to multielement airfoil calculations

Published:1987-06-09 Issue: Volume: Page:
ISSN:
Container-title:8th Computational Fluid Dynamics Conference
language:
Short-container-title:

Author:

WIGTON LAURENCE¹

Affiliation:

1. Boeing Commercial Airplane Co., Seattle, WA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1987-1142

Reference12 articles.

1. "Newton Solution of Steady Two-DimensionalTransonicFlow," M. B. Giles, PhD thesis submittedto theDepartment of Aeronautics and Astronauticsat MIT,June 1985.

2. "Two-Dimensional Transonic Aerodynamic Design and Analysis Using the Euler Equations," M. Drela, PhD thesis submitted to theDepartment of Aeronautics and Astronauticsat MIT,December 1985.

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