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基于无源合成双射流的百公斤级飞行器短距起降增升首飞验证

罗振兵 王春强 郭芷妍 龚建宇 赵志杰

航空学报2026,Vol.47Issue(13):49-59,11.
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航空学报2026,Vol.47Issue(13):49-59,11.DOI:10.7527/S1000-6893.2026.33291

基于无源合成双射流的百公斤级飞行器短距起降增升首飞验证

First flight test of passive dual synthetic jet for short takeoff and landing lift enhancement

罗振兵 1王春强 1郭芷妍 1龚建宇 1赵志杰1

作者信息

  • 1. 国防科技大学 空天科学学院,长沙 410073
  • 折叠

摘要

Abstract

Active flow control,which dynamically manipulates flow structures by injecting energy into the flow field,presents an innovative strategy to fulfill the high-lift requirements for aircraft operating under Short Takeoff and Landing(STOL)conditions.To assess its practical efficacy,this study developed an integrated control system that combines dual synthetic jet actuators-designed to control flow separation on control surfaces-with a multi-stage circulation control system aimed at augmenting wing lift.This system was deployed on an aircraft platform featuring a 5 m wingspan and a takeoff mass of 100 kilogram class for flight testing.The flight test in November 2025 results revealed that the dual synthetic jet lift-enhancement system significantly improved takeoff and landing performance:the takeoff rotation speed decreased from 26 m/s to 21 m/s,the ground roll distance was reduced from 156 m to 101 m,and the landing touch-down speed declined from 25 m/s to 20 m/s,and the landing energy was lowered by 36%.Furthermore,the achieve-ment of a stable roll rate of 3.8(°)/s through asymmetric actuation directly demonstrates the capacity of system to generate asymmetric lift and rolling control moments via precise flow manipulation.This work represents the first flight validation of a passive dual synthetic jet lift-enhancement technology on a medium-scale aircraft platform,thereby of-fering an innovative,efficient,and independently controllable technical approach for advancing aircraft STOL capabilities.

关键词

合成双射流/短距起降/飞行试验/主动流动控制/增升

Key words

dual synthetic jets/short takeoff and landing/flight test/active flow control/lift enhancement

分类

航空航天

引用本文复制引用

罗振兵,王春强,郭芷妍,龚建宇,赵志杰..基于无源合成双射流的百公斤级飞行器短距起降增升首飞验证[J].航空学报,2026,47(13):49-59,11.

基金项目

国家自然科学基金联合基金(U2141252) (U2141252)

国家自然科学基金创新群体(T2221002) (T2221002)

国家自然科学基金(12572318,12572274) Joint Fund of the National Natural Science Foundation of China(U2141252) (12572318,12572274)

The Innovative Research Group Project of National Natural Science Foundation of China(T2221002) (T2221002)

National Natural Science Foundation of China(12572318,12572274) (12572318,12572274)

航空学报

1000-6893

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