Unsteady Flow and Aerodynamic Noise Analysis Around JAXA Landing Gear Model by Building-Cube Method
Author:
Affiliation:
1. Tohoku University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1081
Reference16 articles.
1. Computational Aeroacoustics Validation and Analysis of a Nose Landing Gear
2. Reprint of: Towards Noise Prediction for Rudimentary Landing Gear
3. Prediction of Flap-Edge Noise Using STAR-CD
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