Advanced Topics in Science and Technology in China - Hypersonic Curved Compression Inlet and Its Inverse Design
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Published By Springer Singapore

9789811507267, 9789811507274

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Features and Drag Reduction Analysis of Drag in Hypersonic Inlet

Advanced Topics in Science and Technology in China - Hypersonic Curved Compression Inlet and Its Inverse Design ◽

10.1007/978-981-15-0727-4_9 ◽

2020 ◽

pp. 281-325

Author(s):

Kunyuan Zhang

Keyword(s):

Drag Reduction ◽

Hypersonic Inlet

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Inverse Design of Axisymmetric Basic Flow Field on Basis of Specified Wall Aerodynamic Parameters

Advanced Topics in Science and Technology in China - Hypersonic Curved Compression Inlet and Its Inverse Design ◽

10.1007/978-981-15-0727-4_6 ◽

2020 ◽

pp. 163-212

Author(s):

Kunyuan Zhang

Keyword(s):

Flow Field ◽

Basic Flow ◽

Inverse Design ◽

Aerodynamic Parameters

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Forward Design of Two Dimensional Curved Shock Wave Curved Compression Surface

Advanced Topics in Science and Technology in China - Hypersonic Curved Compression Inlet and Its Inverse Design ◽

10.1007/978-981-15-0727-4_3 ◽

2020 ◽

pp. 61-96

Author(s):

Kunyuan Zhang

Keyword(s):

Shock Wave ◽

Two Dimensional

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The Development of Curved Compression and Its Application Prospect

Advanced Topics in Science and Technology in China - Hypersonic Curved Compression Inlet and Its Inverse Design ◽

10.1007/978-981-15-0727-4_10 ◽

2020 ◽

pp. 327-330

Author(s):

Kunyuan Zhang

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Introduction

Advanced Topics in Science and Technology in China - Hypersonic Curved Compression Inlet and Its Inverse Design ◽

10.1007/978-981-15-0727-4_1 ◽

2020 ◽

pp. 1-37

Author(s):

Kunyuan Zhang

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Inverse Design and Experiment of Hypersonic Curved Shock Wave Compression Inlet

Advanced Topics in Science and Technology in China - Hypersonic Curved Compression Inlet and Its Inverse Design ◽

10.1007/978-981-15-0727-4_7 ◽

2020 ◽

pp. 213-251

Author(s):

Kunyuan Zhang

Keyword(s):

Shock Wave ◽

Inverse Design ◽

Wave Compression ◽

Shock Wave Compression

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Calculation and Analysis Method of Two Dimensional Curved Shock Wave Curved Compression Flow Field

Advanced Topics in Science and Technology in China - Hypersonic Curved Compression Inlet and Its Inverse Design ◽

10.1007/978-981-15-0727-4_2 ◽

2020 ◽

pp. 39-59

Author(s):

Kunyuan Zhang

Keyword(s):

Shock Wave ◽

Flow Field ◽

Two Dimensional ◽

Analysis Method ◽

Compression Flow

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Concept of Hypersonic Adaptive Variable Geometric Curved Compression Inlet

Advanced Topics in Science and Technology in China - Hypersonic Curved Compression Inlet and Its Inverse Design ◽

10.1007/978-981-15-0727-4_8 ◽

2020 ◽

pp. 253-279

Author(s):

Kunyuan Zhang

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Inverse Design of Curved Shock Wave Compression Surface on Basis of Specified Wall Aerodynamic Parameters

Advanced Topics in Science and Technology in China - Hypersonic Curved Compression Inlet and Its Inverse Design ◽

10.1007/978-981-15-0727-4_5 ◽

2020 ◽

pp. 125-161

Author(s):

Kunyuan Zhang

Keyword(s):

Shock Wave ◽

Inverse Design ◽

Wave Compression ◽

Aerodynamic Parameters ◽

Shock Wave Compression

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Inverse Design of Compression Channel with Specified Exit Aerodynamic Parameters

Advanced Topics in Science and Technology in China - Hypersonic Curved Compression Inlet and Its Inverse Design ◽

10.1007/978-981-15-0727-4_4 ◽

2020 ◽

pp. 97-124

Author(s):

Kunyuan Zhang

Keyword(s):

Inverse Design ◽

Aerodynamic Parameters

Download Full-text

Advanced Topics in Science and Technology in China - Hypersonic Curved Compression Inlet and Its Inverse DesignLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By Springer Singapore

Features and Drag Reduction Analysis of Drag in Hypersonic Inlet

Inverse Design of Axisymmetric Basic Flow Field on Basis of Specified Wall Aerodynamic Parameters

Forward Design of Two Dimensional Curved Shock Wave Curved Compression Surface

The Development of Curved Compression and Its Application Prospect

Introduction

Inverse Design and Experiment of Hypersonic Curved Shock Wave Compression Inlet

Calculation and Analysis Method of Two Dimensional Curved Shock Wave Curved Compression Flow Field

Concept of Hypersonic Adaptive Variable Geometric Curved Compression Inlet

Inverse Design of Curved Shock Wave Compression Surface on Basis of Specified Wall Aerodynamic Parameters

Inverse Design of Compression Channel with Specified Exit Aerodynamic Parameters

Advanced Topics in Science and Technology in China - Hypersonic Curved Compression Inlet and Its Inverse Design
Latest Publications