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Numerical Solutions for the Cawapi Configuration on Unstructured Grids at KTH/FOI, Sweden: Part II
FOI.
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering.
2009 (English)In: Understanding and Modeling Vortical Flows to Improve the Technology Readiness Level for Military Aircraft, 2009Chapter in book (Other academic)
Abstract [en]

This article represents a second contribution of the Swedish Defence Research Agency, FOI, and the Royal Institute of Technology, KTH, to the Cranked-Arrow Wing Aerodynamics Project International, CAWAPI. The main focus of this article is on evaluation of the effect of different formulation of boundary conditions on the engine mass flow and resulting wing upper surface pressures.

Place, publisher, year, edition, pages
2009.
Series
NATO RTO Technical Report, AVT-113
National Category
Engineering and Technology
Identifiers
URN: urn:nbn:se:kth:diva-25342OAI: oai:DiVA.org:kth-25342DiVA: diva2:357520
Note
QC 20101018Available from: 2010-10-18 Created: 2010-10-18Bibliographically approved

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CiteExportLink to record
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