偏转矢量喷流对双三角翼前缘涡破裂影响的实验研究

本文应用染色液流动显示技术对后缘偏转喷流情况下76°/40°双三角翼前缘涡破裂位置的变化进行了观测,实验结果表明偏转喷流主要推迟与喷流方向相同一侧前缘涡的破裂,而使另一侧前缘涡破裂略有提前.随着喷流偏转角度的增大,喷流使两前缘涡破裂位置差逐渐增大.另外,随着模型攻角的增大,前缘涡涡核与双三角翼翼面的夹角逐渐增大,导致偏转喷流的作用逐渐减弱.     

三角翼上分离及涡流的数值模拟

综述了三角翼(包括双三角翼,边条-三角翼,近距耦合鸭翼)上分离及涡流问题的数值模拟进展,介绍了用Euler方程、N-S方程的数值方法模拟不同三角翼,在不同攻角、不同来流M数等多种条件下的复杂涡流形态和流动结构,研究了控制方程、网格、湍流模型和计算方法等对计算结果的影响。      

高升力外形下机翼的位流计算

本文采用第二代低阶面元法给出了一种高升力外形外机翼位流计算方法。     

Line shape in far wings and water vapor absorption in a broad temperature interval

Despite the long-term history of extensive studies on water vapor continuum absorption it can hardly be said that an exhaustive consideration has been given to this problem both from experimental and theoretical viewpoints. For instance, deficiency remains concerning the precise data on the absorption coefficient as a function of temperature, especially at reduced temperatures. New experimental data on water vapor continuum absorption in the 800-1250 cm⁻¹ spectral region at temperatures from 311 to 363 K have become available quite recently [15]. Two advanced variants of the line wing theory - asymptotic and quasistatic - are briefly outlined. The asymptotic line wing theory has been used successfully to describe the absorption coefficient both at elevated temperatures of the Baranov study and at the temperatures of earlier experimental data. Comparison is made with the results obtained from the quasistatic line wing theory.     

80°/65°双三角翼摇滚特性风洞实验研究

介绍了在FL-23高速风洞中研究自由摇滚的装置、试验方法、数据采集等试验技术.在马赫数从0.3到0.6范围内,对应的雷诺数从0.56×107/m至1.126×107/m范围内,开展了双三角翼大迎角下的摇滚特性的研究,包括迎角、马赫数、初始释放等参数的影响,给出了典型的结果.结果表明,随着模型迎角的增加,双三角翼呈现不同的滚转运动形态,包括静态稳定、准极限环摇滚、双周期震荡等;试验中马赫数提高对翼摇滚起抑制作用;摇滚运动的最终平衡状态和摇滚幅值与初始状态无关.     

Incomplete Delta Functions

By applying projection operators to state vectors of coordinates, we obtain subspaces in which these states are no longer normalized according to Dirac's delta function but normalized according to what we call incomplete delta functions. We show that this class of functions satisfy identities similar to those satisfied by the Dirac delta function. The incomplete delta functions may be employed advantageously in projected subspaces and in the link between functions defined on the whole space and the projected subspace. We apply a similar procedure to finite-dimensional vector spaces for which we define incomplete Kronecker deltas. Dispersion relations for the momenta are obtained and sums over poles are defined and obtained with the aid of differences of incomplete delta functions.     

改进的红外辐射-量热法测量O2(1△)绝对浓度

The absolute O2 （1Δ）concentration measurement performed for a singlet oxygen generator（SOG）by using the infrared radiation-calorimetry method is reported with a detailed discussion of its principle and related technique. The influence of O2 （1Δ）gas temperature variation is considered and the corresponding correction has been made,which is neglected by the previous researchers and may cause a significant error in the case of measurement for the large O2 （1Δ）flowrate. Furthermore,an automatically balanced Wheatstone bridge circuit,which is necessary for O2 （1Δ）detection on the SOG of short operation period,is designed and tested by measuring the heat capacity of oxygen. The final error analyses give out a total relative error of ±16% for the O2 （1Δ）concentration,which mainly arises from the measurements of infrared radiation,pressure and temperature at the optical cell.     

Two-photon exchange to proton electromagnetic properties in time-like region

The contributions of two-photon exchange in the process e~+ + e~-→p +(p) including N and △ intermediate states are estimated in a simple hadronic model. The corrections to the unpolarized cross section as well as to the polarized observables P_x and P_z are evaluated. The results show the corrections to unpolarized cross section are small and the angle dependence becomes weak at small s after considering the N and △(1232) contributions simultaneously, while the correction to P_z is enhanced.