In contrast , the regular and good reserved delta front is disadvantaged to form fluxoturbidite.

相反,形规则、保存完好的角洲前缘反而不利于滑塌浊积岩的形成。

Seismicity can damage the stability of delta front and form liquefied fluxoturbidite and faulted fluxoturbidite.

其中地震作用可以角洲前缘的稳定性，形成液化滑塌浊积体和断阶滑塌浊积体。

Loss of anterior ertebral height, degree of kyphotic deformity, and percentage retropulsion were recorded at seeral phases of treatment.

在几个治疗阶段记录椎体前缘高度、驼背畸形的程度、后退步的百分比等。

Reserves geological and microtectonics fe ature play important control function of remnant oil distribution.Taking the Se ries as a whole, it is eviden...

从整个层系看前缘席状砂微相始终控制着剩余油储量,应作为挖潜的重点之一。

The key reason for the improved performance are the pairs of counterrotating swirls created at either side of the leading-edge bumps, called tubercles.

隆起前缘能增进性能的关键，因为在这些隆起节瘤的两侧，会产生成对的反向旋转涡流。

Two patterns of air plane engine inlet hot-air anti-icer are introduced in this paper, one is circumferential anti-icer, the other is double skin corrugated chord direction anti-icer.

摘要飞机发动机防冰对飞行安全具有十分重要的意义，对于热气防冰系统，前缘防冰器的结构型式对防冰的效果影响很大。

In contrast , the regular and good reserved delta front is disadvantaged to form fluxoturbidite.

相,形规则、保存完好的三角洲而不利于滑塌浊积岩的形成。

Seismicity can damage the stability of delta front and form liquefied fluxoturbidite and faulted fluxoturbidite.

其中地震作用可以破坏三角洲的稳定性，形成液化滑塌浊积体和断阶滑塌浊积体。

Loss of anterior ertebral height, degree of kyphotic deformity, and percentage retropulsion were recorded at seeral phases of treatment.

在几个治疗阶段记录椎体高度、驼背畸形的程度、后退步的百分比等。

Reserves geological and microtectonics fe ature play important control function of remnant oil distribution.Taking the Se ries as a whole, it is eviden...

从整个层系看席状砂微相始终控制着剩余油储量,应作为挖潜的重点之一。

The key reason for the improved performance are the pairs of counterrotating swirls created at either side of the leading-edge bumps, called tubercles.

隆起能增进性能的关键理由，是因为在这些隆起节瘤的两侧，会产生成对的向流。

Two patterns of air plane engine inlet hot-air anti-icer are introduced in this paper, one is circumferential anti-icer, the other is double skin corrugated chord direction anti-icer.

摘要飞机发动机防冰对飞行安全具有十分重要的意义，对于热气防冰系统，防冰器的结构型式对防冰的效果影响很大。

In contrast , the regular and good reserved delta front is disadvantaged to form fluxoturbidite.

相反,规则、保存完好三角洲前缘反而不利于滑塌浊积成。

Seismicity can damage the stability of delta front and form liquefied fluxoturbidite and faulted fluxoturbidite.

其中地震作用可以破坏三角洲前缘稳定性，成液化滑塌浊积体和断阶滑塌浊积体。

Loss of anterior ertebral height, degree of kyphotic deformity, and percentage retropulsion were recorded at seeral phases of treatment.

在几个治疗阶段记录椎体前缘高度、驼背畸程度、后退步百分比等。

Reserves geological and microtectonics fe ature play important control function of remnant oil distribution.Taking the Se ries as a whole, it is eviden...

从整个层系看前缘席状砂微相始终控制着剩余油储量,应作为挖潜重点之一。

The key reason for the improved performance are the pairs of counterrotating swirls created at either side of the leading-edge bumps, called tubercles.

隆起前缘能增进性能关键理由，是因为在这些隆起节瘤，会产生成对反向旋转涡流。

Two patterns of air plane engine inlet hot-air anti-icer are introduced in this paper, one is circumferential anti-icer, the other is double skin corrugated chord direction anti-icer.

摘要飞机发动机防冰对飞行安全具有十分重要意义，对于热气防冰系统，前缘防冰器结构型式对防冰效果影响很大。

In contrast , the regular and good reserved delta front is disadvantaged to form fluxoturbidite.

相反,形规则、保存完好的三角洲前缘反而不利于滑塌浊积岩的形成。

Seismicity can damage the stability of delta front and form liquefied fluxoturbidite and faulted fluxoturbidite.

其中地震以破坏三角洲前缘的稳定性，形成液化滑塌浊积体和断阶滑塌浊积体。

Loss of anterior ertebral height, degree of kyphotic deformity, and percentage retropulsion were recorded at seeral phases of treatment.

几个治疗阶段记录椎体前缘高度、驼背畸形的程度、后退步的百分比等。

Reserves geological and microtectonics fe ature play important control function of remnant oil distribution.Taking the Se ries as a whole, it is eviden...

从整个层系看前缘席状砂微相始终控制着剩余油储量,应挖潜的重点之一。

The key reason for the improved performance are the pairs of counterrotating swirls created at either side of the leading-edge bumps, called tubercles.

隆起前缘能增进性能的关键理由，是因些隆起节瘤的两侧，会产生成对的反向旋转涡流。

Two patterns of air plane engine inlet hot-air anti-icer are introduced in this paper, one is circumferential anti-icer, the other is double skin corrugated chord direction anti-icer.

摘要飞机发动机防冰对飞行安全具有十分重要的意义，对于热气防冰系统，前缘防冰器的结构型式对防冰的效果影响很大。

In contrast , the regular and good reserved delta front is disadvantaged to form fluxoturbidite.

相反,规则、保存完好三角洲前缘反而不利于滑塌浊积岩成。

Seismicity can damage the stability of delta front and form liquefied fluxoturbidite and faulted fluxoturbidite.

其中地震作用可以破坏三角洲前缘稳定性，成液化滑塌浊积体和断阶滑塌浊积体。

Loss of anterior ertebral height, degree of kyphotic deformity, and percentage retropulsion were recorded at seeral phases of treatment.

在几个治疗阶段记录椎体前缘高度、驼背畸度、后退步百分比。

Reserves geological and microtectonics fe ature play important control function of remnant oil distribution.Taking the Se ries as a whole, it is eviden...

个层系看前缘席状砂微相始终控制着剩余油储量,应作为挖潜重点之一。

The key reason for the improved performance are the pairs of counterrotating swirls created at either side of the leading-edge bumps, called tubercles.

隆起前缘能增进性能关键理由，是因为在这些隆起节瘤两侧，会产生成对反向旋转涡流。

Two patterns of air plane engine inlet hot-air anti-icer are introduced in this paper, one is circumferential anti-icer, the other is double skin corrugated chord direction anti-icer.

摘要飞机发动机防冰对飞行安全具有十分重要意义，对于热气防冰系统，前缘防冰器结构型式对防冰效果影响很大。

In contrast , the regular and good reserved delta front is disadvantaged to form fluxoturbidite.

,形规则、保存完好的三角洲前缘而不利于滑塌浊积岩的形成。

Seismicity can damage the stability of delta front and form liquefied fluxoturbidite and faulted fluxoturbidite.

其中地震作用可以破坏三角洲前缘的稳定性，形成液化滑塌浊积体和断阶滑塌浊积体。

Loss of anterior ertebral height, degree of kyphotic deformity, and percentage retropulsion were recorded at seeral phases of treatment.

在几个治疗阶段记录椎体前缘高度、驼背畸形的程度、后退步的百分比等。

Reserves geological and microtectonics fe ature play important control function of remnant oil distribution.Taking the Se ries as a whole, it is eviden...

从整个层系看前缘席状砂微始终控制着剩余油储量,应作为挖潜的重点之一。

The key reason for the improved performance are the pairs of counterrotating swirls created at either side of the leading-edge bumps, called tubercles.

隆起前缘能增进性能的关键理由，是因为在这些隆起节瘤的两侧，会产生成对的向旋转涡流。

Two patterns of air plane engine inlet hot-air anti-icer are introduced in this paper, one is circumferential anti-icer, the other is double skin corrugated chord direction anti-icer.

摘要飞机发动机防冰对飞具有十分重要的意义，对于热气防冰系统，前缘防冰器的结构型式对防冰的效果影响很大。

In contrast , the regular and good reserved delta front is disadvantaged to form fluxoturbidite.

相反,形规则、保存完好的三角洲前缘反而不利于塌浊积岩的形成。

Seismicity can damage the stability of delta front and form liquefied fluxoturbidite and faulted fluxoturbidite.

其中地震作用可以破坏三角洲前缘的稳定性，形成塌浊积体和断阶塌浊积体。

Loss of anterior ertebral height, degree of kyphotic deformity, and percentage retropulsion were recorded at seeral phases of treatment.

在几个治疗阶段记录椎体前缘高度、驼背畸形的程度、后退步的百分比等。

Reserves geological and microtectonics fe ature play important control function of remnant oil distribution.Taking the Se ries as a whole, it is eviden...

从整个层系看前缘席状砂微相始终控制着剩余油储量,应作为挖潜的重点之。

The key reason for the improved performance are the pairs of counterrotating swirls created at either side of the leading-edge bumps, called tubercles.

前缘能增进性能的关键理由，是因为在这些节瘤的两侧，会产生成对的反向旋转涡流。

Two patterns of air plane engine inlet hot-air anti-icer are introduced in this paper, one is circumferential anti-icer, the other is double skin corrugated chord direction anti-icer.

摘要飞机发动机防冰对飞行安全具有十分重要的意义，对于热气防冰系统，前缘防冰器的结构型式对防冰的效果影响很大。

In contrast , the regular and good reserved delta front is disadvantaged to form fluxoturbidite.

相反,形规则、保存完好三角洲前缘反而不利于滑塌浊积岩形成。

Seismicity can damage the stability of delta front and form liquefied fluxoturbidite and faulted fluxoturbidite.

其中地震作用可以破坏三角洲前缘稳定性，形成液化滑塌浊积体和断阶滑塌浊积体。

Loss of anterior ertebral height, degree of kyphotic deformity, and percentage retropulsion were recorded at seeral phases of treatment.

在几个治疗阶段记录椎体前缘高度、驼背畸形程度、后退步百分比等。

Reserves geological and microtectonics fe ature play important control function of remnant oil distribution.Taking the Se ries as a whole, it is eviden...

从整个层系看前缘席状砂微相始终控制着剩余油储量,应作为挖潜点之一。

The key reason for the improved performance are the pairs of counterrotating swirls created at either side of the leading-edge bumps, called tubercles.

隆起前缘能增进性能关键理由，是因为在这些隆起节瘤两侧，会产生成对反向旋转涡流。

Two patterns of air plane engine inlet hot-air anti-icer are introduced in this paper, one is circumferential anti-icer, the other is double skin corrugated chord direction anti-icer.

摘飞机发动机防冰对飞行安全具有十分意义，对于热气防冰系统，前缘防冰器结构型式对防冰效果影响很大。

In contrast , the regular and good reserved delta front is disadvantaged to form fluxoturbidite.

相反,规则、保存完好三角洲前缘反而不利于滑塌浊积岩。

Seismicity can damage the stability of delta front and form liquefied fluxoturbidite and faulted fluxoturbidite.

中地震作用可以破坏三角洲前缘稳定性，液化滑塌浊积体和断阶滑塌浊积体。

Loss of anterior ertebral height, degree of kyphotic deformity, and percentage retropulsion were recorded at seeral phases of treatment.

在几个治疗阶段记录椎体前缘高度、驼背畸程度、后退步百分比等。

Reserves geological and microtectonics fe ature play important control function of remnant oil distribution.Taking the Se ries as a whole, it is eviden...

从整个层系看前缘席状砂微相始终控制着剩余油储量,应作为挖潜重点之一。

The key reason for the improved performance are the pairs of counterrotating swirls created at either side of the leading-edge bumps, called tubercles.

隆起前缘能增进性能关键理由，是因为在这些隆起两侧，会产生对反向旋转涡流。

Two patterns of air plane engine inlet hot-air anti-icer are introduced in this paper, one is circumferential anti-icer, the other is double skin corrugated chord direction anti-icer.

摘要飞机发动机防冰对飞行安全具有十分重要意义，对于热气防冰系统，前缘防冰器结构型式对防冰效果影响很大。

In contrast , the regular and good reserved delta front is disadvantaged to form fluxoturbidite.

相反,形规则、保存完好三角洲前缘反而不塌浊积岩形。

Seismicity can damage the stability of delta front and form liquefied fluxoturbidite and faulted fluxoturbidite.

其中地震作用可以破坏三角洲前缘稳定性，形液化塌浊积体和断阶塌浊积体。

Loss of anterior ertebral height, degree of kyphotic deformity, and percentage retropulsion were recorded at seeral phases of treatment.

在几个治疗阶段记录椎体前缘高度、驼背畸形程度、后退步百分比等。

Reserves geological and microtectonics fe ature play important control function of remnant oil distribution.Taking the Se ries as a whole, it is eviden...

从整个层系看前缘席状砂微相始终控制着剩余油储量,应作为挖潜重点之一。

The key reason for the improved performance are the pairs of counterrotating swirls created at either side of the leading-edge bumps, called tubercles.

隆起前缘能增进性能关键理由，是因为在这些隆起节瘤两侧，会产生反向旋转涡流。

Two patterns of air plane engine inlet hot-air anti-icer are introduced in this paper, one is circumferential anti-icer, the other is double skin corrugated chord direction anti-icer.

摘要飞机发动机防冰飞行安全具有十分重要意义，热气防冰系统，前缘防冰器结构型式防冰效果影响很大。