An Effective Computation Method Based on Field Velocity Approach for Acceleration Derivative
Jun Yang, Yu Qian
Available Online August 2013.
- 10.2991/icacsei.2013.76How to use a DOI?
- Field velocity, CFD, acceleration derivative, numerical simulation, unsteady flow.
A novel method of calculating static derivatives and acceleration derivatives using Computational Fluid Dynamics is presented. This method uses field velocity approach to simulate the unsteady forced-plunging flow field over the aircraft without updating the field grids during each time step. This provides an improvement in computational efficiency over similar precision without loss of generality. Finally, to verify the present method, the Basic Finner missile as the benchmark example was taken to calculate its acceleration derivatives at various Mach number. Results are in fairly good agreement with traditionally method and the tunnel experimental results. Comparisons with the results of time-dependent simulations are also included.
- © 2013, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Jun Yang AU - Yu Qian PY - 2013/08 DA - 2013/08 TI - An Effective Computation Method Based on Field Velocity Approach for Acceleration Derivative BT - Proceedings of the 2013 International Conference on Advanced Computer Science and Electronics Information (ICACSEI 2013) PB - Atlantis Press SP - 304 EP - 306 SN - 1951-6851 UR - https://doi.org/10.2991/icacsei.2013.76 DO - 10.2991/icacsei.2013.76 ID - Yang2013/08 ER -