E-LIB Suche - Ergebnisse für: Zheng-yin Ye

1

The interference aerodynamics caused by the wing elasticity..:

Lei, Yang ; Zheng-yin, Ye
Acta Astronautica. 121 (2016) - p. 116-129 , 2016

Link: https://doi.org/10.1016/..

2

Mechanism of single-mode panel flutter in low supersonic fl..:

Ye, Liu-qing ; Ye, Kun ; Jin, Ke..
Aerospace Science and Technology. 147 (2024) - p. 109002 , 2024

Link: https://doi.org/10.1016/..

3

Sensitivity and uncertainty analysis of the nonlinear fligh..:

Qiao, Chen-Liang ; Xu, He-Yong ; Ye, Zheng-Yin
Aerospace Science and Technology. 139 (2023) - p. 108389 , 2023

Link: https://doi.org/10.1016/..

4

Research on Aerothermoelasticity for Hypersonic Inlet with ..:

Kun YE ; Yi-fan ZHANG ; Zheng-yin YE
http://qtwl.xml-journal.net/cn/article/doi/10.19527/j.cnki.2096-1642.1053. , 2023

Link: https://doi.org/10.19527..

5

Aeroelastic stability and nonlinear flutter analysis of vis..:

Ye, Liu-qing ; Ye, Zheng-yin ; Ye, Kun.
Aerospace Science and Technology. 117 (2021) - p. 106909 , 2021

Link: https://doi.org/10.1016/..

6

Theoretical analysis for the effect of static pressure diff..:

Ye, Liu-qing ; Ye, Zheng-yin
Aerospace Science and Technology. 109 (2021) - p. 106428 , 2021

Link: https://doi.org/10.1016/..

7

A low-boom and low-drag design method for supersonic aircra..:

Ye, Liu-qing ; Ye, Zheng-yin ; Ye, Kun..
Advances in Aerodynamics. 3 (2021) 1 - p. , 2021

Link: https://doi.org/10.1186/..

8

A low-boom and low-drag design method for supersonic aircra..:

Liu-qing Ye ; Zheng-yin Ye ; Kun Ye..
https://doi.org/10.1186/s42774-021-00079-6. , 2021

Link: https://doi.org/10.1186/..

9

Inflatable Leading Edge-Based Dynamic Stall Control conside..:

Xing, Shi-Long ; Xu, He-Yong ; Ma, Ming-Sheng.
International Journal of Aerospace Engineering. 2020 (2020) - p. 1-28 , 2020

Link: https://doi.org/10.1155/..

10

Design and Optimization Method for Hypersonic Quasi-Waverid..:

Liu, Wen ; Zhang, Chen-An ; Wang, Fa-Min.
AIAA Journal. 58 (2020) 5 - p. 2132-2146 , 2020

Link: https://doi.org/10.2514/..

11

Inflatable Leading Edge-Based Dynamic Stall Control conside..:

Shi-Long Xing ; He-Yong Xu ; Ming-Sheng Ma.
http://dx.doi.org/10.1155/2020/9046542. , 2020

Link: https://doi.org/10.1155/..

12

ILES, DDES and URANS Simulations of the Separated Flow Arou..:

, In: Lecture Notes in Electrical Engineering; The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018),

Xu, He-Yong ; Dong, Qing-Li ; Qiao, Chen-Liang. - p. 746-777 , 2019

Link: https://doi.org/10.1007/..

13

Flow Control over the Blunt Trailing Edge of Wind Turbine A..:

Xu, He-Yong ; Dong, Qing-Li ; Qiao, Chen-Liang.
Energies. 11 (2018) 3 - p. 619 , 2018

Link: https://doi.org/10.3390/..

14

Effects of Shock Location on Aeroelastic Stability of Flexi..:

Ye, Liu-Qing ; Ye, Zheng-Yin
AIAA Journal. 56 (2018) 9 - p. 3732-3744 , 2018

Link: https://doi.org/10.2514/..

15

Active Circulation Control on the Blunt Trailing Edge Wind ..:

Xu, He-Yong ; Qiao, Chen-Liang ; Yang, Hui-Qiang.
AIAA Journal. 56 (2018) 2 - p. 554-570 , 2018

Link: https://doi.org/10.2514/..