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61.
CFD理论黏性流场中三维振动水翼的非定常水动力性能(英文) 总被引:1,自引:0,他引:1
The motion of the fins and control surfaces of underwater vehicles in a fluid is an interesting and challenging research subject.
Typically the effect of fin oscillations on the fluid flow around such a body is highly unsteady, generating vortices and
requiring detailed analysis of fluid-structure interactions. An understanding of the complexities of such flows is of interest
to engineers developing vehicles capable of high dynamic performance in their propulsion and maneuvering. In the present study,
a CFD based RANS simulation of a 3-D fin body moving in a viscous fluid was developed. It investigated hydrodynamic performance
by evaluating the hydrodynamic coefficients (lift, drag and moment) at two different oscillating frequencies. A parametric
analysis of the factors that affect the hydrodynamic performance of the fin body was done, along with a comparison of results
from experiments. The results of the simulation were found in close agreement with experimental results and this validated
the simulation as an effective tool for evaluation of the unsteady hydrodynamic coefficients of 3-D fins. This work can be
further be used for analysis of the stability and maneuverability of fin actuated underwater vehicles. 相似文献
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研究了抗坏血酸对CH2(COOH)2-BrO3^--Mn^2+-H2SO4体系化学振荡反应的影响,考察了该体系中各反应物的初始浓度范围及主要影响因素.结果表明:在5.7×10^-4~8.5×10^-2mol/L的范围内,抗坏血酸对振荡反应的诱导期有较大影响,且抗坏血酸的浓度与振幅及抗坏血酸浓度的对数与诱导期倒数的对数均存在良好线形关系.诱导期和周期的表观活化参数分别为56.63kJ/mol,73.81kJ/mol;同时还对抗坏血酸参与下可能振荡反应机理进行了探讨. 相似文献
64.
为了研究飞机的三角翼前缘涡破裂后,破裂涡流的非定常特性,在风洞中进行了75°后掠三角翼的动态测压实验.实验结果表明:三角翼翼面的压力脉动强度变化和翼面上前缘涡的流态是正相关的,在前缘涡破裂迎角区,上翼面的压力脉动强度最高达到33 Pa,抖振强度随迎角的变化趋势与上翼面的压力脉动随迎角的变化趋势相同.通过对压力信号的分析得出,三角翼翼面上的压力脉动主要是由破裂涡流中的螺旋波引起的,螺旋波产生了三角翼机翼抖振. 相似文献
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航母关键系统对架次率的影响研究 总被引:1,自引:0,他引:1
航母舰载机的出动架次率是衡量航母及其航空联队作战能力的基本标准,是航母重要的战技指标。本文着重探讨了航母关键系统对架次率的影响,分析了弹射装置、着舰引导系统、飞机升降机、航空弹药贮运系统的能力对舰载机出动架次率的直接影响,对比了常规动力航母和核动力航母的加速性能对架次率的间接作用。 相似文献
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The unsteady flow of viscoelastic fluid in a cylindrical pipe was investigated using the fractional Maxwell model. Two special cases of unsteady pipe flow were expressed. The first is start-up flow, and the second is oscillating flow. The exact solution of start-up flow under a constant pressure gradient was obtained by using the theories of Laplace transform and Fourier-Bessel series for fractional derivatives. The exact solution of oscillating flow was obtained by utilizing the separation of variables. 相似文献