Transonic aeroelastic computations of a delta wing configuration with high fidelity equations

Hiroshi Terashima; Kenji Ono

doi:10.1007/978-3-540-92779-2-133

Transonic aeroelastic computations of a delta wing configuration with high fidelity equations

Hiroshi Terashima, Kenji Ono

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Original language	English
Title of host publication	Computational Fluid Dynamics 2006 - Proceedings of the Fourth International Conference on Computational Fluid Dynamics, ICCFD 2006
Publisher	springer berlin
Pages	843-848
Number of pages	6
DOIs	https://doi.org/10.1007/978-3-540-92779-2-133
Publication status	Published - 2009
Externally published	Yes
Event	4th International Conference on Computational Fluid Dynamics, ICCFD 2006 - Ghent, Belgium Duration: Jul 10 2006 → Jul 14 2006

Other

Other	4th International Conference on Computational Fluid Dynamics, ICCFD 2006
Country/Territory	Belgium
City	Ghent
Period	7/10/06 → 7/14/06

All Science Journal Classification (ASJC) codes

Fluid Flow and Transfer Processes

Access to Document

10.1007/978-3-540-92779-2-133

Cite this

Transonic aeroelastic computations of a delta wing configuration with high fidelity equations. / Terashima, Hiroshi; Ono, Kenji.
Computational Fluid Dynamics 2006 - Proceedings of the Fourth International Conference on Computational Fluid Dynamics, ICCFD 2006. springer berlin, 2009. p. 843-848.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Terashima, H & Ono, K 2009, Transonic aeroelastic computations of a delta wing configuration with high fidelity equations. in Computational Fluid Dynamics 2006 - Proceedings of the Fourth International Conference on Computational Fluid Dynamics, ICCFD 2006. springer berlin, pp. 843-848, 4th International Conference on Computational Fluid Dynamics, ICCFD 2006, Ghent, Belgium, 7/10/06. https://doi.org/10.1007/978-3-540-92779-2-133

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AU - Ono, Kenji

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BT - Computational Fluid Dynamics 2006 - Proceedings of the Fourth International Conference on Computational Fluid Dynamics, ICCFD 2006

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T2 - 4th International Conference on Computational Fluid Dynamics, ICCFD 2006

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ER -

Transonic aeroelastic computations of a delta wing configuration with high fidelity equations

Other

All Science Journal Classification (ASJC) codes

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Cite this