Aeroelastic Analysis for Aeropropulsion Applications

by National Aeronautics and Space Administration

Aeroelastic codes with advanced capabilities for modeling flow require substantial computational time. On the other hand, fast-running linear aeroelastic codes lack the capability to model three-dimensional, transonic, vortical, and viscous flows. The goal of this work was to develop an aeroelastic code with accurate modeling capabilities and small computational requirements. Keith, Theo G., Jr. and Bakhle, Milind A. Glenn Research Center

30 pages, Paperback

Published June 19, 2018

About the author

The National Aeronautics and Space Administration (NASA) is an independent agency of the U.S. federal government responsible for the civil space program, aeronautics research, and space research.