A Multi-Fidelity Approach for Aerodynamic Performance Computations of Formation Flight

A Multi-Fidelity Approach for Aerodynamic Performance Computations of Formation Flight

This paper introduces a multi-fidelity computational framework for the analysis of aerodynamic performance of flight formation. The Vortex Lattice and Reynolds Averaged Navier–Stokes methods form the basis of the framework, as low- and high-fidelity, respectively. Initially, the computatio...

Full description

Bibliographic Details
Main Authors: Diwakar Singh, Antonios F. Antoniadis, Panagiotis Tsoutsanis, Hyo-Sang Shin, Antonios Tsourdos, Samuel Mathekga, Karl W. Jenkins
Format: Article
Language:English
Published: MDPI AG 2018-06-01
Series:Aerospace
Subjects:
multi-fidelity
aerodynamic performance
formation
VLM
RANS
Online Access:http://www.mdpi.com/2226-4310/5/2/66

Internet

http://www.mdpi.com/2226-4310/5/2/66

Similar Items