An overview of recent progress regarding the computational aeroelastic and aeroservoelastic (ASE) analyses of a low-boom supersonic configuration is presented. The overview includes details of the computational models developed to date with a focus on unstructured CFD grids, computational aeroelastic analyses, sonic boom propagation studies that include static aeroelastic effects, and gust loads analyses. In addition, flutter boundaries using aeroelastic Reduced-Order Models (ROMs) are presented at various Mach numbers of interest. Details regarding a collaboration with the Royal Institute of Technology (KTH, Stockholm, Sweden) to design, fabricate, and test a full-span aeroelastic wind-tunnel model are also presented.
A Status Review of the Commercial Supersonic Technology (CST) Aeroservoelasticity (ASE) Project
AIAA Aviation 2016 ; 2016 ; Washington, DC, United States
2016-06-13
Conference paper
No indication
English
British Library Conference Proceedings | 2016
|NTIS | 1990
|NTRS | 1993
|Wiley | 2014
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