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The Latest Progress in the Computational Aerodynamic System for Practical Aircraft Configurations
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English
Abstract
An aerodynamic simulation system for practical aircraft configurations has been developed. The outline of the system is first described, and then its recent progress is presented especially for a grid generation as well as a newly introduced parallel vector computer at the National Aerospace Laboratory, Japan.
Some of computational results using the new simulation system are also presented for a transonic aircraft and a Space-Plane.
Authors
Citation
Takanashi, S. and Takemoto, M., "The Latest Progress in the Computational Aerodynamic System for Practical Aircraft Configurations," SAE Technical Paper 940061, 1994, https://doi.org/10.4271/940061.Also In
References
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