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Fixed Wing Aero Buildup Runbook | Skills Pool

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Fixed Wing Aero Buildup Runbook

执行固定翼气动阻力分解计算。当需要从几何参数计算详细阻力清单时调用。

BaiSongt4 Sterne12.02.2026

Beruf: Aerospace Engineers
Kategorien: Debugging

Skill-Inhalt

固定翼气动阻力分解执行步骤（Runbook）

角色定位（统一入口）

本技能默认由 fixed_wing_overall_sizing_runbook 在“收敛后的阶段 2–7 扩展分析”中自动执行（Stage2 Aero）。
单独调用用于回答两类问题：
- “我填的 initial_guess.cd0 是否合理？如果不合理，哪一部分在贡献阻力？”
- “能否用几何可追溯的 CD0 替代拍脑袋的 CD0？”

计算模型（以代码为准）

部件级 buildup：aircraft_design/aero_drag_buildup.py
- 输出 cd0 及 Fuselage/Wing/Horizontal Tail/Vertical Tail/Misc/Wave Drag 分解

输入要点（来自统一输入 JSON）

requirements.cruise_altitude_m、requirements.cruise_mach：巡航工况
initial_guess.thickness_ratio、initial_guess.sweep_deg、initial_guess.aspect_ratio、initial_guess.taper_ratio

Verwandte Skills

Schnellinstallation

Fixed Wing Aero Buildup Runbook

npx skillvault add BaiSongt/baisongt-aircraft-design-skill-trae-skills-02-class2-preliminary-aero-buildup-runbook-skill-md

Skill herunterladen Repository öffnen

Autor: BaiSongt
Sterne: 4
Aktualisiert: 12.02.2026
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01固定翼气动阻力分解执行步骤（Runbook）

几何（优先级从高到低）：

geometry_shape / geometry_detailed（最可追溯）
若未提供，则由总体闭环的几何派生模块给出默认量级

执行方式

统一入口运行：fixed_wing_overall_sizing_runbook
重点关注收敛后是否进入扩展阶段（未收敛则不会生成阻力分解结果）

输出位置与读取

output/<project>_*/advanced_design_results_*.json：
- stage2_aero.cd0、stage2_aero.cd0_breakdown、stage2_aero.wave_drag
output/<project>_*/advanced_design_report.md：可读的阻力分解表

常见诊断

cd0 明显过大：优先检查机身尺度（长度/直径）与 thickness_ratio
波阻占比异常：检查巡航 Mach 与后掠/厚度比是否匹配
机翼/尾翼占比异常：检查面积比（尾翼相对翼面积）与外形细化输入是否缺失

02

角色定位（统一入口）

03计算模型（以代码为准）

04输入要点（来自统一输入 JSON）

06输出位置与读取

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Aerospace Engineers