惯性力导数对飞行载荷弹性修正的影响研究

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中图分类号：V215.3 文献标志码：A 文章编号：2095-2945（2026）03-0094-04

Abstract：Inthedesignofaireraftflightloadelasticcoretion，inertialforcederivativesarecloselyrelatedtoparameters suchasflightMachnumber，altitude，ircraftstiffsscharacterisics，andmassdistrbutionThecalcultioninvolesmayconditions，isverytime-consumingandthevaluesareusuallysmallandoftenneglectedinflightloadelasticcoectionTispaper discusesthecalculationofinertialforederivativesandtheirappicationinloadcorrctioninstaticaeroelasticanalsis.Taking theloadelasticcorectionofalargecivilaircraftasanexample，theinfluenceofinertialforcederivativesonloadelasticcorctionisanalyzed.Numericalexamplesshowthatinertialfocederivativeshavecertainefectsonaiaftflightloadcoioand should not be ignored.

Keywords：aeroelasticity； flight loads；staticaeroelasticity; inertial force derivatives; load correction

静气动弹性研究的主要问题是弹性变形对升力面载荷分布的影响，当飞行速度比较低时，弹性变形的影响较小。（剩余4040字）