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，形成液化滑体和断阶滑体。

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理由，是因为在这些隆起节瘤的两侧，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、驼背畸形、后退步百分。

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

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,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,形规则、保存完好三角洲前缘反而不利于滑塌浊形成。

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，形成液化滑塌浊体和断阶滑塌浊体。

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，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.

在几治疗阶段记录椎体前缘高度、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理由，是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,形规则、保存完好的三角洲前缘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理由，是因为在这些隆起节瘤的两侧，会产生成对的转涡流。

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、保存完好的三角洲前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，前防冰器的结构型式对防冰的效果影响很大。