Study on Flight Load Modeling Method for Complex Structure Aircraft
The traditional flight load modeling method of complex structure aircraft has the problems of large error and low efficiency. A flight load improved modeling method is proposed,which is comprehensively considering the influence of the bridge index and load equation index on the load model. Taking th...
| Main Authors: | , , |
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| Format: | Article |
| Language: | zho |
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Editorial Department of Advances in Aeronautical Science and Engineering
2022-04-01
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| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2021139?st=article_issue |
| _version_ | 1811166383937945600 |
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| author | CHEN Zhiming TANG Ning FAN Huafei |
| author_facet | CHEN Zhiming TANG Ning FAN Huafei |
| author_sort | CHEN Zhiming |
| collection | DOAJ |
| description | The traditional flight load modeling method of complex structure aircraft has the problems of large error and low efficiency. A flight load improved modeling method is proposed,which is comprehensively considering the influence of the bridge index and load equation index on the load model. Taking the multi-beam and multi-wall structure as an example,the load model based on the wing ground load calibration test data of a certain type of aircraft is built. The bending moment and shearing force of improved method and traditional method are compared.The model obtained by the improved method is verified with flight test data. The results show that the flight load improved modeling method is suitable for the load modeling of complex structure aircraft. The improved method can improve the accuracy and iterative stability of the load model while processing ground test data and the load model obtained by the improved method can be used for flight load measurement and safety monitoring. |
| first_indexed | 2024-04-10T15:52:30Z |
| format | Article |
| id | doaj.art-252da0ad3ea84b7cac03ed18b23d334e |
| institution | Directory Open Access Journal |
| issn | 1674-8190 |
| language | zho |
| last_indexed | 2024-04-10T15:52:30Z |
| publishDate | 2022-04-01 |
| publisher | Editorial Department of Advances in Aeronautical Science and Engineering |
| record_format | Article |
| series | Hangkong gongcheng jinzhan |
| spelling | doaj.art-252da0ad3ea84b7cac03ed18b23d334e2023-02-11T02:26:00ZzhoEditorial Department of Advances in Aeronautical Science and EngineeringHangkong gongcheng jinzhan1674-81902022-04-01132455010.16615/j.cnki.1674-8190.2022.02.0720220207Study on Flight Load Modeling Method for Complex Structure AircraftCHEN Zhiming0TANG Ning1FAN Huafei2Aircraft Institute, Chinese Flight Test Establishment, Xi'an 710089, ChinaAircraft Institute, Chinese Flight Test Establishment, Xi'an 710089, ChinaAircraft Institute, Chinese Flight Test Establishment, Xi'an 710089, ChinaThe traditional flight load modeling method of complex structure aircraft has the problems of large error and low efficiency. A flight load improved modeling method is proposed,which is comprehensively considering the influence of the bridge index and load equation index on the load model. Taking the multi-beam and multi-wall structure as an example,the load model based on the wing ground load calibration test data of a certain type of aircraft is built. The bending moment and shearing force of improved method and traditional method are compared.The model obtained by the improved method is verified with flight test data. The results show that the flight load improved modeling method is suitable for the load modeling of complex structure aircraft. The improved method can improve the accuracy and iterative stability of the load model while processing ground test data and the load model obtained by the improved method can be used for flight load measurement and safety monitoring.http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2021139?st=article_issueflight testflight loadcomplex structure aircraftload model |
| spellingShingle | CHEN Zhiming TANG Ning FAN Huafei Study on Flight Load Modeling Method for Complex Structure Aircraft Hangkong gongcheng jinzhan flight test flight load complex structure aircraft load model |
| title | Study on Flight Load Modeling Method for Complex Structure Aircraft |
| title_full | Study on Flight Load Modeling Method for Complex Structure Aircraft |
| title_fullStr | Study on Flight Load Modeling Method for Complex Structure Aircraft |
| title_full_unstemmed | Study on Flight Load Modeling Method for Complex Structure Aircraft |
| title_short | Study on Flight Load Modeling Method for Complex Structure Aircraft |
| title_sort | study on flight load modeling method for complex structure aircraft |
| topic | flight test flight load complex structure aircraft load model |
| url | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2021139?st=article_issue |
| work_keys_str_mv | AT chenzhiming studyonflightloadmodelingmethodforcomplexstructureaircraft AT tangning studyonflightloadmodelingmethodforcomplexstructureaircraft AT fanhuafei studyonflightloadmodelingmethodforcomplexstructureaircraft |