Free flight wind tunnel test similarity law derivation for light store separation from aircraft

Based on the linear displacement motion similarity and angular displacement motion similarity, the similarity law for free flight test of light store separation from aircraft is deduced. The problem that the ideal test model is too light to be processed and the free flight separation test in wind tu...

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Main Authors: Fei Xue, Han Qin, Yuchao Wang, Zenghui Jiang, Xin Jin, Peng Bai
Format: Article
Language:English
Published: SAGE Publishing 2019-05-01
Series:Advances in Mechanical Engineering
Online Access:https://doi.org/10.1177/1687814019853062
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spelling doaj-7ce4dc0ae96947be9433fa4762e704862020-11-25T02:52:30ZengSAGE PublishingAdvances in Mechanical Engineering1687-81402019-05-011110.1177/1687814019853062Free flight wind tunnel test similarity law derivation for light store separation from aircraftFei Xue0Han Qin1Yuchao Wang2Zenghui Jiang3Xin Jin4Peng Bai5China Academy of Aerospace Aerodynamics, Beijing, ChinaChina Academy of Aerospace Aerodynamics, Beijing, ChinaChina Academy of Aerospace Aerodynamics, Beijing, ChinaChina Academy of Aerospace Aerodynamics, Beijing, ChinaAVIC Chengdu Aircraft Design & Research Institute, Chengdu, ChinaChina Academy of Aerospace Aerodynamics, Beijing, ChinaBased on the linear displacement motion similarity and angular displacement motion similarity, the similarity law for free flight test of light store separation from aircraft is deduced. The problem that the ideal test model is too light to be processed and the free flight separation test in wind tunnel is harder to achieve due to the model scaling is solved. The new similarity law was simplified reasonably, and the relationship equation between separation velocity and model mass was obtained. The wind-loaded state is simulated by computational fluid dynamics, and the real separation data of aircraft, the separation data of previous test methods, and the simulation data of different mass and different separation velocity trajectories of this similarity law are obtained. The improved effect of the new similarity law is verified by data comparison. The results show that by properly increasing the mass of wind tunnel test model, the difficulty of wind tunnel test can be greatly reduced while the separation trajectory is similar, and the angular displacement error can be guaranteed to be within acceptable range. In order to ensure better consistency between flight and free flight wind tunnel test, it solves the problem that similarity law can only be designed but cannot be realized.https://doi.org/10.1177/1687814019853062
collection DOAJ
language English
format Article
sources DOAJ
author Fei Xue
Han Qin
Yuchao Wang
Zenghui Jiang
Xin Jin
Peng Bai
spellingShingle Fei Xue
Han Qin
Yuchao Wang
Zenghui Jiang
Xin Jin
Peng Bai
Free flight wind tunnel test similarity law derivation for light store separation from aircraft
Advances in Mechanical Engineering
author_facet Fei Xue
Han Qin
Yuchao Wang
Zenghui Jiang
Xin Jin
Peng Bai
author_sort Fei Xue
title Free flight wind tunnel test similarity law derivation for light store separation from aircraft
title_short Free flight wind tunnel test similarity law derivation for light store separation from aircraft
title_full Free flight wind tunnel test similarity law derivation for light store separation from aircraft
title_fullStr Free flight wind tunnel test similarity law derivation for light store separation from aircraft
title_full_unstemmed Free flight wind tunnel test similarity law derivation for light store separation from aircraft
title_sort free flight wind tunnel test similarity law derivation for light store separation from aircraft
publisher SAGE Publishing
series Advances in Mechanical Engineering
issn 1687-8140
publishDate 2019-05-01
description Based on the linear displacement motion similarity and angular displacement motion similarity, the similarity law for free flight test of light store separation from aircraft is deduced. The problem that the ideal test model is too light to be processed and the free flight separation test in wind tunnel is harder to achieve due to the model scaling is solved. The new similarity law was simplified reasonably, and the relationship equation between separation velocity and model mass was obtained. The wind-loaded state is simulated by computational fluid dynamics, and the real separation data of aircraft, the separation data of previous test methods, and the simulation data of different mass and different separation velocity trajectories of this similarity law are obtained. The improved effect of the new similarity law is verified by data comparison. The results show that by properly increasing the mass of wind tunnel test model, the difficulty of wind tunnel test can be greatly reduced while the separation trajectory is similar, and the angular displacement error can be guaranteed to be within acceptable range. In order to ensure better consistency between flight and free flight wind tunnel test, it solves the problem that similarity law can only be designed but cannot be realized.
url https://doi.org/10.1177/1687814019853062
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AT hanqin freeflightwindtunneltestsimilaritylawderivationforlightstoreseparationfromaircraft
AT yuchaowang freeflightwindtunneltestsimilaritylawderivationforlightstoreseparationfromaircraft
AT zenghuijiang freeflightwindtunneltestsimilaritylawderivationforlightstoreseparationfromaircraft
AT xinjin freeflightwindtunneltestsimilaritylawderivationforlightstoreseparationfromaircraft
AT pengbai freeflightwindtunneltestsimilaritylawderivationforlightstoreseparationfromaircraft
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