Aerostructural optimization of a low sweep transonic wing with shock control bump

Conference paper (2016)

Authors

A. Elham Flight Performance and Propulsion - Aerospace Engineering
B Timmer External organisation
Research Group
Flight Performance and Propulsion (Aerospace Engineering) (TU Delft)
More Info
expand_more

Published Date

2016

Language

English

Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Faculty

Aerospace Engineering

Department

Flow Physics and Technology

Research Group

Flight Performance and Propulsion