High Fidelity, High Order, Large Eddy Simulations of a Real Geometry Aircraft Nose Landing Gear on Hybrid Unstructured Meshes & Small-scale Many-core Computing System
Author:
Affiliation:
1. Cambridge Flow Solutions Ltd
2. BoXeR Solutions KK
3. Cambridge University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0555
Reference12 articles.
1. Preliminary Analysis of Acoustic Measurements from the NASA-Gulfstream Airframe Noise Flight Test
2. Application of FUN3D Solver for Aeroacoustic Simulation of a Nose Landing Gear Configuration
3. Aeroacoustic Simulation of Nose Landing Gear on Adaptive Unstructured Grids with FUN3D
4. Flow simulation system based on high order space-time extension of flux reconstruction method
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1. Efficient and affordable high order, high fidelity Large Eddy Simulations for industrial level applications;55th AIAA Aerospace Sciences Meeting;2017-01-05
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