Open Access
| Issue |
JNWPU
Volume 40, Number 2, April 2022
|
|
|---|---|---|
| Page(s) | 401 - 406 | |
| DOI | https://doi.org/10.1051/jnwpu/20224020401 | |
| Published online | 03 June 2022 | |
- 中国人民解放军总装备部军标发行部 军用飞机结构强度规范第7部分: 气动弹性[S]. GJB 67.7A-2008 [Google Scholar]
- COLE S R, NOLL T E, PERRY B. Transonic dynamic tunnel aeroelastic testing in support of aircraft development[J]. Journal of Aircraft, 2003, 40(5): 820–831 [Article] [CrossRef] [Google Scholar]
- DOGGETT R V. A bibliography of transonic dynamic tunnel(TDT) publications[R]. NASA TM-2016-219355 [Google Scholar]
- GUO Hongtao, YAN Yu, YU Li, et al. Research on flutter test technology of continuously adjusting dynamical pressure in high-speed wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2015, 29(5): 72–77 [Article] (in Chinese) [Google Scholar]
- GUO Hongtao, LU Bo, YU Li, et al. Investigation on full-model flutter of a certain fighter plane in high-speed wind tunnel test[J]. Acta Aeronautica et Astronautica Sinica, 2012, 30(10): 1765–1771 [Article] (in Chinese) [Google Scholar]
- HOU Liangxue, ZHANG Ge, LIU Nan, et al. Transonic flutter based on wind tunnel test model[J]. Journal of Vibration and Shock, 2019, 38(13): 236–241 [Article] (in Chinese) [NASA ADS] [Google Scholar]
- LIU Nan, YI Jianing, WANG Dong, et al. Continuous varying dynamic pressure wind tunnel test method and numerical calculation of flutter characteristics of horizontal tail model[J]. Journal of Vibration and Shock, 2021, 40(15): 11–17 [Article] (in Chinese) [Google Scholar]
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.