网络小展弦比机翼 网络释义 1. 小展弦比机翼 无限小展弦比机翼,vanishing aspect ratio... ... )low-aspect-ratio wing小展弦比机翼) low-aspect wing 小展弦比机翼火> ... www.dictall.com|基于2个网页
4) low-aspect-ratio wing 小展弦比机翼 1. Based on the time-derivative proconditioned method,the low speed aerodynamic propertics of low-aspect-ratio wing are numerically simulated. 以雷诺平均的Navier-Stokes方程为基础,应用非结构混合网格技术,基于有限体积的时间推进预处理方法,对小展弦比机翼的...
1)low-aspect-ratio wing小展弦比机翼 1.Based on the time-derivative proconditioned method,the low speed aerodynamic propertics of low-aspect-ratio wing are numerically simulated.以雷诺平均的Navier-Stokes方程为基础,应用非结构混合网格技术,基于有限体积的时间推进预处理方法,对小展弦比机翼的低速流动进行...
GE Torres,TJ Mueller.Low-aspect-ratio wing aerodynamics at low Reynolds numbers. AIAA Journal . 2004Torres GE and Thomas JM. Low-aspect-ratio wing aerodynamics at low Reynolds numbers. AIAA J 2004; 42: 825-832.Torres GE, Mueller TJ. 2004. Low-aspect-ratio wing aerodynamics at low Reynolds...
This aircraft, a Formula V racer, shows how the configuration is affected by the requirement to fold the wings to lie along the side of the fuselage for transport (in this case tail-first towing). The resulting low aspect ratio wing planform will be ‘draggy’ in high-gturn manoeuvres bu...
The flow over a planar low-aspect-ratio delta wing is considered in the strong viscous-inviscid interaction regime. The study is carried out for Newtonian passage to limit, when the adiabatic exponent tends to unity, while the Mach and Reynolds numbers increase without bound. For the flow over...
The experimental geometry is a low aspect ratio wing, tested in a solid wall wind tunnel. Inflow conditions were measured far enough upstream of the model to allow simple specification. Experimental uncertainties are given for pressure, temperature, velocity, and position measurements, as well as ...
Aerodynamics and lateral stability of low-aspect-ratio wings with dihedral at Low Reynolds numbers Flow separation over the side-edge of the wing, a feat known as the cause of roll stall where roll moment no longer increases with angle of attack, is seen to be affected by both changes in ...
An Airplane Design having a Wing with Fuselage Attached to Each Tip This paper describes the conceptual design of an airplane having a low aspect ratio wing with fuselages that are attached to each wing tip. The concept is ... LM Spearman 被引量: 4发表: 2001年 Investigation on improving ...
Watts, The otter board as a low-aspect ratio wing at high angles of attack; some theoretical aspects, Fisheries Research 3 (1985) 351-372.Patterson RN, Watts KC. The Otter board as a low-aspect- ratio wing at high angles of attack; an experimental study. Fish. Res. 1986; 14: 111-...