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超声速民用飞机最小飞行速度适航标准研究

杨建忠 张晨阳 杨士斌

航空工程进展2026,Vol.17Issue(1):100-107,8.
航空工程进展2026,Vol.17Issue(1):100-107,8.DOI:10.16615/j.cnki.1674-8190.2026.01.10

超声速民用飞机最小飞行速度适航标准研究

Study on minimum flight speed airworthiness standard of supersonic civil aircraft

杨建忠 1张晨阳 1杨士斌1

作者信息

  • 1. 中国民航大学 安全科学与工程学院,天津 300300
  • 折叠

摘要

Abstract

Supersonic civil aircraft has significant changes in aerodynamic layout and design compared to subsonic civil aircraft,which will bring new risks and make some provisions of the current regulations inapplicable.By con-ducting a qualitative analysis of CCAR Part 25 and the special conditions while using computational fluid dynamics(CFD)methods,the aerodynamic characteristics of a small aspect ratio,large sweep angle supersonic civil aircraft in low-speed conditions are analyzed.The safety intent behind the minimum flight speed mentioned in the superson-ic civil aircraft special conditions is revealed through a combination of qualitative and quantitative analysis.The re-sults show that the stall speed reference defined by CCAR Part 25 is not applicable to supersonic civil aircraft.Su-personic civil aircraft adopt the minimum flight speed and zero climb rate speed as new speed references to ensure stable flight while still having climbing ability.

关键词

超声速民用飞机/涡升力/计算流体力学/适航/气动分析/最小飞行速度/零爬升率速度

Key words

supersonic civil aircraft/vortex lift/computational fluid dynamics/airworthiness/aerodynamic analy-sis/minimum flight speed/zero rate of climb speed

分类

航空航天

引用本文复制引用

杨建忠,张晨阳,杨士斌..超声速民用飞机最小飞行速度适航标准研究[J].航空工程进展,2026,17(1):100-107,8.

航空工程进展

1674-8190

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