z-logo
open-access-imgOpen Access
Application of Adjoint Methodology to Supersonic Aircraft Design Using Reversed Equivalent Areas
Author(s) -
Sriram K. Rallabhandi
Publication year - 2013
Publication title -
21st aiaa applied aerodynamics conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2013-2663
Subject(s) - supersonic speed , aerospace engineering , computer science , environmental science , engineering

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom