Review of vortex lattice method for supersonic aircraft design
نویسندگان
چکیده
Abstract There has been a renewed interest in developing environmentally friendly, economically viable, and technologically feasible supersonic transport aircraft reduced order modeling methods can play an important contribution accelerating the design process of these future aircraft. This paper reviews use vortex lattice method (VLM) general aerodynamics subsonic The historical overview is reviewed which indicates this for over century development advancements aerodynamic analysis preference VLM other potential flow-solvers because its low highly efficient computational quick efficient. Developments covering steady, unsteady state, linear non-linear characteristics different wing planform purpose several types optimisation reviewed. For decade classical used multi-objective studies commercial unmanned aerial vehicle’s performance optimisation. was one major flow solvers studying aeroelastic many wings NASA’s mission (SST). preferred means solving large numbers parameters less time, more efficiently, cheaper when compared to conventional CFD lends itself detailed study challenging configuration features civil transport.
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ژورنال
عنوان ژورنال: Journal of the Royal Aeronautical Society
سال: 2023
ISSN: ['2059-6464', '0001-9240']
DOI: https://doi.org/10.1017/aer.2023.25