A summary of NASA's High Speed Aeroservoelasticity (ASE) project is provided with a focus on a low-boom supersonic configuration developed by Lockheed-Martin and referred to as the N+2 configuration. The summary includes details of the computational models developed to date including a linear finite element model (FEM), linear unsteady aerodynamic models, structured and unstructured CFD grids, and discussion of the FEM development including sizing and structural constraints applied to the N+2 configuration. Linear results obtained to date include linear mode shapes and linear flutter boundaries. In addition to the tasks associated with the N+2 configuration, a summary of the work involving the development of AeroPropulsoServoElasticity (APSE) models is also discussed.
The NASA High Speed ASE Project: Computational Analyses of a Low-Boom Supersonic Configuration
AIAA Aerospace Sciences Meeting ; 2014 ; National Harbor, MD, United States
2014-01-13
Conference paper
No indication
English
British Library Conference Proceedings | 2014
|British Library Conference Proceedings | 2015
|