菜单
QA checklist for OpenAeroStruct aero/structures work in open-air. Use when editing or reviewing src/openair/aero/**, src/openair/structures/**, aero.json, structures.json, trim/stability results, or OAS surface dicts.
默认使用会先检查来源的 Prompt；你也可以切换为直接命令，或下载本地副本。
决定是否安装前，请先阅读 SKILL.md，以及 SkillsMP 当前展示的配套文件。
用 Codex 或 Claude 帮你安装 复制这段 Prompt，粘贴到 Codex、Claude 或其他助手里，让它检查 Skill 页面并帮你完成安装。
直接命令不会经过审查 Prompt；运行前请先检查来源。
npx skills add https://github.com/elodin-sys/open-air --skill aero-qa-aerostructures命令会保持在同一行。复制前请横向滚动并检查完整内容。
想先保存到本地？可下载 SkillsMP 当前能够提供的文件。
QA checklist for OpenVSP geometry work in open-air. Use when editing or reviewing src/openair/geometry/**, geometry.json, .vsp3/STL exports, packing, or anything touching the OpenVSP Python API.
QA checklist for OpenMDAO optimization work in open-air. Use when editing or reviewing src/openair/mdo/**, mdo.json, DV bounds, constraints, SLSQP behavior, or the optimized prototype YAML.
AERO QA dispatcher for validating open-air aircraft prototypes. Use whenever reviewing or validating a prototype, a concept design YAML, results/ artifacts, a design report, or any stage output (sizing, geometry, aero, structures, mdo, validation, reporting, TACS, SU2); or when asked to "QA this design", "validate the prototype", or judge whether a design meets desires.md.
正在显示 SKILL.md
| name | aero-qa-aerostructures |
| description | QA checklist for OpenAeroStruct aero/structures work in open-air. Use when editing or reviewing src/openair/aero/**, src/openair/structures/**, aero.json, structures.json, trim/stability results, or OAS surface dicts. |
Read docs/guidebook/03-openaerostruct.md and 09-sizing-aero-buildup.md;
execute their "Check your work" lists.
Non-negotiables for this repo:
<surface>.def_mesh
and aero_states.<surface>_def_mesh) — a missing wing or fallback-htail
connection gives NaN or silently-wrong results from the default mesh.cg input; trim work must reference the real CG from
openair.mission.balance, and the flat VLM needs the thin-airfoil cm_ac
added for cambered sections.aero.json: trim.converged, selected control within ~1° of
spec (tailless washout or fallback-tail incidence), |cm_residual| < 0.005,
and stability.sm_full/.sm_reserve inside the mission band (measured from
dCM/dCL, not the geometric model).failure <= 0 at +4g is the pass criterion (KS of von Mises over
allowable minus 1, safety factor 1.5). W0 excludes wing mass and OAS's
internal fuel burn (keep R tiny).err_on_non_converge=True.num_y odd full-span; symmetric half is the LEFT wing —
j=0 tip, j=-1 root; spanwise CP arrays are tip-first.