Numerical Solutions for the Cawapi Configuration on Unstructured Grids at KTH/FOI, Sweden: Part II
2009 (English)In: Understanding and Modeling Vortical Flows to Improve the Technology Readiness Level for Military Aircraft, 2009Chapter in book (Other academic)
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
, NATO RTO Technical Report, AVT-113
Engineering and Technology
IdentifiersURN: urn:nbn:se:kth:diva-25342OAI: oai:DiVA.org:kth-25342DiVA: diva2:357520
QC 201010182010-10-182010-10-18Bibliographically approved