Unsteady aerodynamics of nonslender delta wings
Unsteady aerodynamics of nonslender delta wings, covering topics of shear layer
instabilities, structure of nonslender vortices, breakdown, maneuvering wings, and …
instabilities, structure of nonslender vortices, breakdown, maneuvering wings, and …
Review of self-induced roll oscillations and its attenuation for low-aspect-ratio wings
T Hu - Proceedings of the Institution of Mechanical Engineers …, 2019 - journals.sagepub.com
Micro aerial vehicles are currently receiving growing interest because of their broad
applications in many fields. In their flight tests, the onset of unwanted large amplitude roll …
applications in many fields. In their flight tests, the onset of unwanted large amplitude roll …
Vortex dynamics of free-to-roll slender and nonslender delta wings
UNSTEADY aerodynamics of delta wings in roll motion are important for various
applications including high-speed civil transport, spacecraft, fighter aircraft, unmanned …
applications including high-speed civil transport, spacecraft, fighter aircraft, unmanned …
Effect of geometric variations on the wing rock of blended wing–body aircraft
Blended wing–body configurations are anticipated to dominate future transport and military
aerospace designs. The departure of the conventional tube-wing configuration has opened …
aerospace designs. The departure of the conventional tube-wing configuration has opened …
The self-excited rolling oscillations induced by fore-body vortices
BF Ma, XY Deng, Z Rong, B Wang - Aerospace Science and Technology, 2015 - Elsevier
The self-excited oscillation of a wing body induced by fore-body vortices was studied
experimentally. To avoid interference, the experimental procedure is divided into two steps …
experimentally. To avoid interference, the experimental procedure is divided into two steps …
Effect of slenderness ratio on free-to-roll wing aerodynamics
MANNED fighter aircraft and unmanned combat air vehicles may require high angle-of-
attack maneuvers where the roll dynamics become crucial. Small unmanned air vehicles …
attack maneuvers where the roll dynamics become crucial. Small unmanned air vehicles …
Wing Rock Induced by a Hemisphere–Cylinder Forebody
LK Wei, BF Ma - Journal of Aircraft, 2014 - arc.aiaa.org
The wing rock induced by a hemisphere–cylinder forebody was investigated experimentally
using an isolated delta wing and wing body. For the delta wing with sweep angle of 30 deg …
using an isolated delta wing and wing body. For the delta wing with sweep angle of 30 deg …
[HTML][HTML] Experimental investigation of influence of strake wings on self-induced roll motion at high angles of attack
X Geng, Z Shi, K Cheng - Chinese Journal of Aeronautics, 2016 - Elsevier
The modern high performance air vehicles are required to have extreme maneuverability,
which includes the ability of controlled maneuvers at high angle of attack. However, the …
which includes the ability of controlled maneuvers at high angle of attack. However, the …
大攻角运动时的机翼摇滚问题研究综述
刘伟， 杨小亮， 张涵信， 邓小刚 - 力学进展, 2008 - lxjz.cstam.org.cn
机翼摇滚是现代战斗机, 导弹设计中普遍遇到的横向不稳定现象之一, 属于典型的大攻角动态
特性问题. 20 多年来, 机翼摇滚问题在国内外航空工业界, 学术界都引起了极大的重视和兴趣 …
特性问题. 20 多年来, 机翼摇滚问题在国内外航空工业界, 学术界都引起了极大的重视和兴趣 …
A study on dynamic characteristics of delta wing in rolling motion near ground
H Kawazoe, T Yorikane, Y Tone - 39th Aerospace Sciences Meeting …, 2001 - arc.aiaa.org
Dynamic properties of aerodynamic force and moment acting on a delta wing were
experimentally studied in a wind tunnel. Its flight attitude changes smoothly and periodically …
experimentally studied in a wind tunnel. Its flight attitude changes smoothly and periodically …