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。

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

地震作用可以破坏三角洲前缘的稳定性，形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.

隆前缘能增进性能的关键理由，是因为在这些隆的两侧，会产生对的反向旋转涡流。

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.

摘要动防冰对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.

前缘能增进性能的关键理由，是因为在这节瘤的两侧，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缘、背畸形的程、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，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.

其中地震用可以破坏三角洲前缘的稳定性，形成液化浊积体和断浊积体。

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,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.

在几个治疗阶段记录椎体前缘高、驼背畸形的程、步的等。

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，对于热气防冰系统，前缘防冰器的结构型式对防冰的效果影响很大。