Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Bin Bin Lv"'
Publikováno v:
Applied Mechanics and Materials. :1187-1190
This paper by taking the hypersonic speed wing surface as the research object, according to the basic theory of thermal mode analysis, calculates and analyzes the influence of temperature variation on model vibration characteristics. According to the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::55a58f45a828669bba23d06b1910f966
https://doi.org/10.4028/www.scientific.net/amm.633-634.1187
https://doi.org/10.4028/www.scientific.net/amm.633-634.1187
Publikováno v:
Advanced Materials Research. :1584-1587
This paper introduces an automatic shutdown system for model protection during the flutter test in high speed wind tunnels. This automatic shutdown system can be used to determine any unsafe condition through model flutter signals before triggering s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::92ec044457a81487b092c8c94e532c2c
https://doi.org/10.4028/www.scientific.net/amr.1030-1032.1584
https://doi.org/10.4028/www.scientific.net/amr.1030-1032.1584
Publikováno v:
Applied Mechanics and Materials. :1233-1236
This paper introduces the solution for calculating the divergence dynamic pressure of wing under subsonic speed based on static aeroelasticity. Several groups of results (q ~ θ values) are calculated and the divergence dynamic pressure can be obtain
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3e1fabe587c8ed8338e9c53ea0ef6a50
https://doi.org/10.4028/www.scientific.net/amm.633-634.1233
https://doi.org/10.4028/www.scientific.net/amm.633-634.1233
Publikováno v:
Advanced Materials Research. :26-29
This paper adopts self-designed wing model to conduct flutter test on subsonic and transonic, and obtains flutter characteristic of the model, and the test results are used for calibration and verification of flutter procedures. The sub-critical extr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fe4ff1a8b139796d9cbc61617b6777c4
https://doi.org/10.4028/www.scientific.net/amr.1006-1007.26
https://doi.org/10.4028/www.scientific.net/amr.1006-1007.26
Publikováno v:
Advanced Materials Research. :328-334
Aiming at the 2.4m×2.4m wind tunnel, this paper introduces the floating suspension system (“FSS”) in the full-mode flutter test, analyzes the impact of the model’s “free” movement to the elastic vibration mode and verifies the control effe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9ff7fd3ed48d933bd34bef9f7ba3e1bd
https://doi.org/10.4028/www.scientific.net/amr.816-817.328
https://doi.org/10.4028/www.scientific.net/amr.816-817.328
Publikováno v:
Applied Mechanics and Materials. 392:170-177
with the BP algorithm, this paper sets up the High angle of attack unsteady aerodynamic neural network model. By using the large-amplitude pitch oscillation dynamic test data of some slender model in high-speed wind tunnel, this paper trains and veri
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0e1984867e6e7733f46a1b1326aa5d84
https://doi.org/10.4028/www.scientific.net/amm.392.170
https://doi.org/10.4028/www.scientific.net/amm.392.170
Publikováno v:
Applied Mechanics and Materials. :2177-2181
For the continuously-varying dynamic pressure flutter test data in the high-speed wind tunnel; this paper analyzes the strengths and weaknesses of the data Processing Method in this field. The data selection and stacking mode is improved. A Butterwor
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dd3abf5ad8757dd3c9c096f8020d5309
https://doi.org/10.4028/www.scientific.net/amm.397-400.2177
https://doi.org/10.4028/www.scientific.net/amm.397-400.2177
Publikováno v:
Advanced Materials Research. :1031-1034
To effectively excite the all moving wing flutter model and limiting or quick locking model in case of bigger amplitude of the model, an excitation and limiting and locking device is designed for the high-speed wind tunnel flutter test model. This pa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::999ed9fbde3b99a0a5dac1b59ad811c4
https://doi.org/10.4028/www.scientific.net/amr.753-755.1031
https://doi.org/10.4028/www.scientific.net/amr.753-755.1031
Autor:
Ying-Chun, Xing, Bin-Bin, Lv, En-Qi, Ye, En-Yuan, Fan, Shi-Yang, Li, Li-Xin, Wang, Chun-Guang, Zhang, Ya-Hui, Zhao
Publikováno v:
Zootaxa. 3962
Brachymystax tsinlingensis Li, 1966 is revalidated and redescribed. It can be distinguished from all congeners by the following combination of characteristics: no spots on operculum; gill rakers 15-20; lateral-line scales 98-116; pyloric caeca 60-71.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=pmid________::795532a146e39eddb67ef2b7577dacb9
https://pubmed.ncbi.nlm.nih.gov/26249386
https://pubmed.ncbi.nlm.nih.gov/26249386
Autor:
Enqi Ye, Shi-Yang Li, Ya-Hui Zhao, Bin-Bin Lv, Yingchun Xing, Chun-Guang Zhang, Li-Xin Wang, En-Yuan Fan
Publikováno v:
Zootaxa. 3962:191
Brachymystax tsinlingensis Li, 1966 is revalidated and redescribed. It can be distinguished from all congeners by the following combination of characteristics: no spots on operculum; gill rakers 15-20; lateral-line scales 98-116; pyloric caeca 60-71.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::942116e42686da4869585b5ec4f036b8
https://doi.org/10.11646/zootaxa.3962.1.12
https://doi.org/10.11646/zootaxa.3962.1.12