{"id":24201257,"url":"https://github.com/lfariello/hypersonic_aerodynamics","last_synced_at":"2026-06-07T08:31:31.732Z","repository":{"id":272325293,"uuid":"916215926","full_name":"Lfariello/Hypersonic_aerodynamics","owner":"Lfariello","description":"Comparison between the flow field around a cone (3D) and a wedge (2D). Analysis of the Taylor-Maccoll flow field within the supersonic boundary layer of a cone at zero angle of attack in a hypersonic flow.","archived":false,"fork":false,"pushed_at":"2025-01-13T17:30:28.000Z","size":18,"stargazers_count":0,"open_issues_count":0,"forks_count":0,"subscribers_count":1,"default_branch":"main","last_synced_at":"2025-01-13T18:27:33.215Z","etag":null,"topics":["aerodynamics","computational-fluid-dynamics","flow-based-programming","hypersonic","iterative-methods","matlab","programming"],"latest_commit_sha":null,"homepage":"","language":"MATLAB","has_issues":true,"has_wiki":null,"has_pages":null,"mirror_url":null,"source_name":null,"license":"apache-2.0","status":null,"scm":"git","pull_requests_enabled":true,"icon_url":"https://github.com/Lfariello.png","metadata":{"files":{"readme":"README.md","changelog":null,"contributing":null,"funding":null,"license":"LICENSE","code_of_conduct":null,"threat_model":null,"audit":null,"citation":null,"codeowners":null,"security":null,"support":null,"governance":null,"roadmap":null,"authors":null,"dei":null,"publiccode":null,"codemeta":null}},"created_at":"2025-01-13T17:10:35.000Z","updated_at":"2025-01-13T17:37:19.000Z","dependencies_parsed_at":"2025-01-13T18:27:36.762Z","dependency_job_id":"9931d803-8e05-4572-9e91-a803246a4a0b","html_url":"https://github.com/Lfariello/Hypersonic_aerodynamics","commit_stats":null,"previous_names":["lfariello/hypersonic_aerodynamics"],"tags_count":0,"template":false,"template_full_name":null,"repository_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/repositories/Lfariello%2FHypersonic_aerodynamics","tags_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/repositories/Lfariello%2FHypersonic_aerodynamics/tags","releases_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/repositories/Lfariello%2FHypersonic_aerodynamics/releases","manifests_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/repositories/Lfariello%2FHypersonic_aerodynamics/manifests","owner_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/owners/Lfariello","download_url":"https://codeload.github.com/Lfariello/Hypersonic_aerodynamics/tar.gz/refs/heads/main","host":{"name":"GitHub","url":"https://github.com","kind":"github","repositories_count":241644642,"owners_count":19996214,"icon_url":"https://github.com/github.png","version":null,"created_at":"2022-05-30T11:31:42.601Z","updated_at":"2022-07-04T15:15:14.044Z","host_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub","repositories_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/repositories","repository_names_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/repository_names","owners_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/owners"}},"keywords":["aerodynamics","computational-fluid-dynamics","flow-based-programming","hypersonic","iterative-methods","matlab","programming"],"created_at":"2025-01-13T21:14:59.570Z","updated_at":"2026-06-07T08:31:31.685Z","avatar_url":"https://github.com/Lfariello.png","language":"MATLAB","funding_links":[],"categories":[],"sub_categories":[],"readme":"# Hypersonic_aerodynamics\nComparison between the flow field around a cone (3D) and a wedge (2D). Analysis of the Taylor-Maccoll flow field within the supersonic boundary layer of a cone at zero angle of attack in a hypersonic flow.  \nResults are compared with those obtained for a wedge under the same asymptotic conditions.  \nThe associated function (AngoloUrto.m) is able to calculate the shock angle using the Newton-Raphson method (iterative method).  \nThe input and output angles are expressed in degrees.  \nThe other associated function (TaylorMaccoll.m) is able to solve the hypersonic conical flow field by integrating  the Taylor-Maccoll equations using the direct method. The function takes as input the asymptotic conditions and the flow deflection angle (in radians)  \nand returns the thermo-fluid dynamic conditions within the shock layer.\n","project_url":"https://awesome.ecosyste.ms/api/v1/projects/github.com%2Flfariello%2Fhypersonic_aerodynamics","html_url":"https://awesome.ecosyste.ms/projects/github.com%2Flfariello%2Fhypersonic_aerodynamics","lists_url":"https://awesome.ecosyste.ms/api/v1/projects/github.com%2Flfariello%2Fhypersonic_aerodynamics/lists"}