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Kunyuan Zhang

Nanjing University of Aeronautics and Astronautics

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Concept of Hypersonic Adaptive Variable Geometric Curved Compression Inlet

2020
- Kunyuan Zhang
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Inverse Design of Curved Shock Wave Compression Surface on Basis of Specified Wall Aerodynamic Parameters

2020
- Kunyuan Zhang
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Inverse Design and Experiment of Hypersonic Curved Shock Wave Compression Inlet

2020
- Kunyuan Zhang
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The Experimental and Numerical Study of the Over-Under TBCC Exhaust System

2011
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The Design and Experimental Study of a Multi- Diaphragm Piezoelectric Synthetic Jet Actuator

2007
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