Design and Applications of Preliminary Evaluation Platform of Aerodynamic Forces for Supersonic/Hypersonic Vehicles

Rapid evaluation of aerodynamic forces is a key technology in conceptual and preliminary performance assessment and design optimization for supersonic/hypersonic vehicles, which is expected to achieve a balance between accuracy and time. In this paper, the preliminary evaluation platform of aerodyna...

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Format: Article
Language:zho
Published: EDP Sciences 2018-12-01
Series:Xibei Gongye Daxue Xuebao
Subjects:
Online Access:https://www.jnwpu.org/articles/jnwpu/pdf/2018/06/jnwpu2018366p1076.pdf
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collection DOAJ
description Rapid evaluation of aerodynamic forces is a key technology in conceptual and preliminary performance assessment and design optimization for supersonic/hypersonic vehicles, which is expected to achieve a balance between accuracy and time. In this paper, the preliminary evaluation platform of aerodynamic forces is built based on the physical theories and engineering methods. This platform computes the local velocity vector by using the streamline tracing technology, and extracts the pressure and friction coefficients by calling methods in method database. Furthermore, an example based on HL-20 is brought out. A good agreement is obtained by comparing the calculated results via CFD with the experimental. Also, a good angle of attack compatibility of streamline tracing technology is concluded. This platform has a computation time less than that via CFD and an flight range greater than that via wind tunnel. Finally, the simple flight dynamics simulation is taken out and the synergetic process is verified.
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spelling doaj.art-c321bf45f7c6486090bde8545c2a280f2023-12-03T04:38:28ZzhoEDP SciencesXibei Gongye Daxue Xuebao1000-27582609-71252018-12-013661076108410.1051/jnwpu/20183661076jnwpu2018366p1076Design and Applications of Preliminary Evaluation Platform of Aerodynamic Forces for Supersonic/Hypersonic VehiclesRapid evaluation of aerodynamic forces is a key technology in conceptual and preliminary performance assessment and design optimization for supersonic/hypersonic vehicles, which is expected to achieve a balance between accuracy and time. In this paper, the preliminary evaluation platform of aerodynamic forces is built based on the physical theories and engineering methods. This platform computes the local velocity vector by using the streamline tracing technology, and extracts the pressure and friction coefficients by calling methods in method database. Furthermore, an example based on HL-20 is brought out. A good agreement is obtained by comparing the calculated results via CFD with the experimental. Also, a good angle of attack compatibility of streamline tracing technology is concluded. This platform has a computation time less than that via CFD and an flight range greater than that via wind tunnel. Finally, the simple flight dynamics simulation is taken out and the synergetic process is verified.https://www.jnwpu.org/articles/jnwpu/pdf/2018/06/jnwpu2018366p1076.pdfhypersonic vehicleaerodynamic forcerapid evaluationplatformstreamline tracingsynergetic simulation
spellingShingle Design and Applications of Preliminary Evaluation Platform of Aerodynamic Forces for Supersonic/Hypersonic Vehicles
Xibei Gongye Daxue Xuebao
hypersonic vehicle
aerodynamic force
rapid evaluation
platform
streamline tracing
synergetic simulation
title Design and Applications of Preliminary Evaluation Platform of Aerodynamic Forces for Supersonic/Hypersonic Vehicles
title_full Design and Applications of Preliminary Evaluation Platform of Aerodynamic Forces for Supersonic/Hypersonic Vehicles
title_fullStr Design and Applications of Preliminary Evaluation Platform of Aerodynamic Forces for Supersonic/Hypersonic Vehicles
title_full_unstemmed Design and Applications of Preliminary Evaluation Platform of Aerodynamic Forces for Supersonic/Hypersonic Vehicles
title_short Design and Applications of Preliminary Evaluation Platform of Aerodynamic Forces for Supersonic/Hypersonic Vehicles
title_sort design and applications of preliminary evaluation platform of aerodynamic forces for supersonic hypersonic vehicles
topic hypersonic vehicle
aerodynamic force
rapid evaluation
platform
streamline tracing
synergetic simulation
url https://www.jnwpu.org/articles/jnwpu/pdf/2018/06/jnwpu2018366p1076.pdf