VISUALIZATION OF INCIDENT OBLIQUE SHOCK WAVE ON SHARP LEADING-EDGE AND SURFACES WITH RAMPS
This work presents a computational simulation of inviscid air flow, at hypersonic speed, when it encounters a sharp surface with ramps. The objective is to visualize and determine the angles of the incident shock waves and compare them with the results obtained from the theoretical mathematical relationships used to study the formation of plane oblique shock waves. The modeling and simulation was carried out in the academic version of Ansys/Fluent®, considering a two-dimensional geometry.
VISUALIZATION OF INCIDENT OBLIQUE SHOCK WAVE ON SHARP LEADING-EDGE AND SURFACES WITH RAMPS
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DOI: 10.22533/at.ed.317342323019
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Palavras-chave: CFD, Shockwaves, Hypersonic, Thermodynamic Properties.
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Keywords: CFD, Shockwaves, Hypersonic, Thermodynamic Properties.
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Abstract:
This work presents a computational simulation of inviscid air flow, at hypersonic speed, when it encounters a sharp surface with ramps. The objective is to visualize and determine the angles of the incident shock waves and compare them with the results obtained from the theoretical mathematical relationships used to study the formation of plane oblique shock waves. The modeling and simulation was carried out in the academic version of Ansys/Fluent®, considering a two-dimensional geometry.
- Ana Larissa Bezerra Rodrigues
- José Bismark de Medeiros
- Edna Santiago Benta
