Grid generation about high-lift wing configurations

Nirajan Adhikari; D. Stephen Nichols

doi:10.1007/978-3-319-62136-4_2

Grid generation about high-lift wing configurations

Nirajan Adhikari, D. Stephen Nichols

Blanket and Fuel Cycle

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

2 Scopus citations

Abstract

The current guidelines provided by the 3rd AIAA CFD High Lift Prediction Workshop for building unstructured meshes representing high-lift wing configurations are demonstrated and discussed. Specifically, Pointwise grid generation software is used to generate general multi-element unstructured grids about the NASA High Lift Common Research Model and the Japanese Aerospace Exploration Agency Standard Model with and without nacelles and pylons. Several modifications to the guidelines that enhance grid quality are presented. Additionally, the user-defined parameters within Pointwise that govern the mesh generation process are reviewed in detail.

Original language	English
Title of host publication	Numerical Simulation of the Aerodynamics of High-Lift Configurations
Publisher	Springer International Publishing
Pages	9-26
Number of pages	18
ISBN (Electronic)	9783319621364
ISBN (Print)	9783319621357
DOIs	https://doi.org/10.1007/978-3-319-62136-4_2
State	Published - Apr 10 2018

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Grid generation about high-lift wing configurations

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