The purpose of this paper is to assess the accuracy and utility of a new unstructured, inviscid, upwind flow solver for the aerodynamic analysis of two aircraft configurations. The two configurations consist of a low-wing transport with nacelle/pylon on and off, and a generic high-speed civil transport. Computations are made at subsonic and transonic Mach numbers for the low-wing transport and at transonic and low-supersonic speeds for the high-speed civil transport. The results include an assessment of grid sensitivity and provide comparisons with experimental data.
Aerodynamic analysis of complex configurations using unstructured grids
AIAA Applied Aerodynamics Conference
1991-01-01
Conference paper
No indication
English
Aerodynamic Analysis of Complex Configurations Using Unstructured Grids
British Library Conference Proceedings | 1991
|Aerodynamic Computations Using Adaptive Unstructured Grids
Online Contents | 1997
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