分别以NO_3^-和NO-2为氮源,在9个不同N/S值条件下进行厌氧脱氮除硫试验。结果表明:当N/S值>0.67时,硝酸盐体系的出水硫化物浓度均小于1.0 mg/L,硫化物去除率达99%,脱硫速度明显高于亚硝酸盐体系,即N_3^-是脱硫最佳的电子受体。硫化...分别以NO_3^-和NO-2为氮源,在9个不同N/S值条件下进行厌氧脱氮除硫试验。结果表明:当N/S值>0.67时,硝酸盐体系的出水硫化物浓度均小于1.0 mg/L,硫化物去除率达99%,脱硫速度明显高于亚硝酸盐体系,即N_3^-是脱硫最佳的电子受体。硫化物加速了对NO-2的去除,即使将N/S值提高为4,对NO-2的去除率仍高达99%,硫化物是去除NO-2适宜的电子供体。硝酸盐体系的出水单质硫浓度明显高于亚硝酸盐体系,亚硝酸盐不利于单质硫富集。硝酸盐体系的N/S值从0.2增大为1时,大部分的N_3^-被转化为N2(产生氮气14~58 m L);而当硫化物不足时(N/S值从1继续增大为4),NO_3^-不能被全部转化为N2。对于亚硝酸盐体系而言,去除的NO-2基本全部生成N2。当NO-2受限时(N/S值<0.4)产生了大量的N2(48 m L),此时部分进水氨氮可能被去除。硝酸盐、亚硝酸盐体系中,硫化物过量时(N/S值=0.2),电子数的差均较高,分别为59%和66%;二者分别在N/S值为1、2时,电子数的差为零,电子得失达到平衡。展开更多
the establishment of multi-element airfoil in steady and unsteady ground effect N-S equation turbulence model, the S-A model of multi element airfoils during takeoff and landing high attack angle change numerical simu...the establishment of multi-element airfoil in steady and unsteady ground effect N-S equation turbulence model, the S-A model of multi element airfoils during takeoff and landing high attack angle change numerical simulation analysis, the calculation results show that the lower altitude, lift and drag wing angle decreased; the greater the ground the effect is more obvious, the greater the loss of lift. The simulation results show that the lift coefficient is slightly less than that of unsteady numerical simulation, and the drag coefficient is slightly less than that of unsteady numerical simulation. The ground disturbance to the wing not only affects the steady state flow field, but also is closely related to the unsteady aerodynamic performance. The results of this study can provide a reference for the design and flight control of large aircraft wings.展开更多
文摘分别以NO_3^-和NO-2为氮源,在9个不同N/S值条件下进行厌氧脱氮除硫试验。结果表明:当N/S值>0.67时,硝酸盐体系的出水硫化物浓度均小于1.0 mg/L,硫化物去除率达99%,脱硫速度明显高于亚硝酸盐体系,即N_3^-是脱硫最佳的电子受体。硫化物加速了对NO-2的去除,即使将N/S值提高为4,对NO-2的去除率仍高达99%,硫化物是去除NO-2适宜的电子供体。硝酸盐体系的出水单质硫浓度明显高于亚硝酸盐体系,亚硝酸盐不利于单质硫富集。硝酸盐体系的N/S值从0.2增大为1时,大部分的N_3^-被转化为N2(产生氮气14~58 m L);而当硫化物不足时(N/S值从1继续增大为4),NO_3^-不能被全部转化为N2。对于亚硝酸盐体系而言,去除的NO-2基本全部生成N2。当NO-2受限时(N/S值<0.4)产生了大量的N2(48 m L),此时部分进水氨氮可能被去除。硝酸盐、亚硝酸盐体系中,硫化物过量时(N/S值=0.2),电子数的差均较高,分别为59%和66%;二者分别在N/S值为1、2时,电子数的差为零,电子得失达到平衡。
文摘the establishment of multi-element airfoil in steady and unsteady ground effect N-S equation turbulence model, the S-A model of multi element airfoils during takeoff and landing high attack angle change numerical simulation analysis, the calculation results show that the lower altitude, lift and drag wing angle decreased; the greater the ground the effect is more obvious, the greater the loss of lift. The simulation results show that the lift coefficient is slightly less than that of unsteady numerical simulation, and the drag coefficient is slightly less than that of unsteady numerical simulation. The ground disturbance to the wing not only affects the steady state flow field, but also is closely related to the unsteady aerodynamic performance. The results of this study can provide a reference for the design and flight control of large aircraft wings.