High-Accuracy Moving Wall Boundary Conditions for Computational Aeroacoustics
46th, Aerospace sciences meeting AIAA ; 2008 ; Reno, NV
01.01.2008
10 pages
Aufsatz (Konferenz)
Englisch
Aerospace , AIAA , Aeronautics , Astronautics
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Wall Boundary Conditions for High-Order Finite Difference Schemes in Computational Aeroacoustics
British Library Conference Proceedings | 1994
|High Accuracy Algorithms for Computational Aeroacoustics
British Library Conference Proceedings | 1994
|