Summary
The inviscid flow around a Pitot-type air intake has been calculated for a fixed freestream Mach number of 0.8 and three angles of attack (-6°, 0°, +6°). The ratio of static pressures at channel exit and infinity has been held constant. The analysis was carried out for an isolated air intake, i.e. the fuselage is omitted and the splitter plate is extended to an infinite flat plate. The Euler equations written in integral-conservation form are solved by a finite volume method applying a Runge-Kutta scheme with local time-step**. The computational mesh is composed by a set of two-dimensional grids, constructed by a complex transformation combined with the solution of geometric partial differential equations. The main features of the predicted flow fields are described and compared with experimental results for a realistic inlet-fuselage combination.
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References
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© 1982 Springer-Verlag Berlin Heidelberg
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Grashof, J. (1982). Investigation of the Three-Dimensional Transonic Flow around an Air Intake by a Finite-Volume Method for the Euler Equations. In: Haase, W. (eds) Recent Contributions to Fluid Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-81932-2_12
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DOI: https://doi.org/10.1007/978-3-642-81932-2_12
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-81934-6
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