Finite-Volume Method with Transpiration Boundary Conditions for Flow About Oscillating Wings-Reference-Cited by-同舟云学术

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Finite-Volume Method with Transpiration Boundary Conditions for Flow About Oscillating Wings

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
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Author:

Huckriede Kees¹,Koop Arjen¹,Hospers Jacco¹,Hoeijmakers Harry¹

Affiliation:

1. University of Twente

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-866

Reference23 articles.

1. 1R.L.Bisplinghoff,H.Ashley,andR.L.Halfman.Aeroelasticity.Addison-Wesley,1957.

2. 2J.Blazek.ComputationalFluidDynamics:PrinciplesandApplications.Elsevier,2005.

3. 5E.J.Foeth.TheStructureofThree-DimensionalSheetCavitation.PhDthesis,DelftUniversityofTechnology,2008.

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