Prediction and Validation Technologies of Aerodynamic Force and Heat for Hypersonic Vehicle Design
Springer Verlag, Singapore
978-981-336-525-4 (ISBN)
Dr. Min Zhao works at the China Academy of Launch Vehicle Technology (CALT). He began his career at the CALT as an engineer for overall rocket design. He has since successively worked as a research engineer, a senior engineer, a research fellow, a department leader and a chief engineer at the CALT. He also completed his Ph.D. in 2005. He has been engaged in the overall design of aerospace craft for the past 30 years, gathering unique insights into aircraft performance. He has been selected for the National Prize for Progress in Science and Technology (Top Grade) twice, and the Aerospace Merit Award once. Thanks to the support of Tsinghua University, the China Academy of Aerospace Aerodynamic, Institute of Mechanics (CAS) and the CALT, he has conducted extensive research on engineering application technologies.
Development of Hypersonic Aerothermodynamic Technologies.- An Overview of Ground-Flying Calibration Technologies for Hypersonic Vehicle.- Flow over Blunt Body and Drag Reduction Control.- A Functional Based Prediction Method for Hypersonic Aerodynamic Force and Heat.- Numerical Method for Flow Transition Prediction.- Embedded Aerosphere Sensing System.- Advanced Wind Tunnel Measurement Technology.
Erscheinungsdatum | 16.03.2021 |
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Reihe/Serie | Springer Aerospace Technology |
Zusatzinfo | 89 Illustrations, color; 60 Illustrations, black and white; XIV, 247 p. 149 illus., 89 illus. in color. |
Verlagsort | Singapore |
Sprache | englisch |
Original-Titel | GAO CHAO SHENG SU QI DONG LI RE HUAN JING XIN XING YU CE YU YAN ZHENG JI SHU |
Maße | 155 x 235 mm |
Themenwelt | Naturwissenschaften ► Physik / Astronomie ► Thermodynamik |
Technik ► Fahrzeugbau / Schiffbau | |
Technik ► Luft- / Raumfahrttechnik | |
Technik ► Maschinenbau | |
Schlagworte | Aerodynamic Force and Heat • Aerodynamic Heat for Hypersonic Flow • Blunt Body and Drag Reduction Control • Flow Transition Prediction • Ground-Flying Calibration Technologies • Hypersonic Aero-thermodynamic Technologies • Hypersonic Flow • Hypersonic Vehicle design • Prediction and Validation Technologies • Prediction Method • Transition Criteria • Turbulence and Transition Model • Wind Tunnel Test Technology |
ISBN-10 | 981-336-525-0 / 9813365250 |
ISBN-13 | 978-981-336-525-4 / 9789813365254 |
Zustand | Neuware |
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