Overview
- Proposes cutting-edge technologies that can soon be applied in hypersonic vehicle design
- Assesses critical issues in hypersonic vehicle design and offers possible solutions
- Provides an overview of non-contact measurement technologies in the wind tunnel
- Introduces a functional optimization-based data correlation method to determine hypersonic vehicle behavior
Part of the book series: Springer Aerospace Technology (SAT)
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Table of contents (7 chapters)
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Front Matter
Keywords
- Wind Tunnel Test Technology
- Hypersonic Vehicle design
- Prediction and Validation Technologies
- Aerodynamic Force and Heat
- Hypersonic Aero-thermodynamic Technologies
- Hypersonic Flow
- Aerodynamic Heat for Hypersonic Flow
- Ground-Flying Calibration Technologies
- Blunt Body and Drag Reduction Control
- Prediction Method
- Flow Transition Prediction
- Turbulence and Transition Model
- Transition Criteria
About this book
This book provides an overview of advanced prediction and verification technologies for aerodynamics and aerothermodynamics and assesses a number of critical issues in advanced hypersonic vehicle design. Focusing on state-of-the-art theories and promising technologies for engineering applications, it also presents a range of representative practical test cases. Given its scope, the book offers a valuable asset for researchers who are interested in thermodynamics, aircraft design, wind tunnel testing, fluid dynamics and aerothermodynamics research methods, introducing them to inspiring new research topics.
Authors and Affiliations
About the author
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.
Bibliographic Information
Book Title: Prediction and Validation Technologies of Aerodynamic Force and Heat for Hypersonic Vehicle Design
Authors: Min Zhao
Series Title: Springer Aerospace Technology
DOI: https://doi.org/10.1007/978-981-33-6526-1
Publisher: Springer Singapore
eBook Packages: Engineering, Engineering (R0)
Copyright Information: National Defense Industry Press 2021
Hardcover ISBN: 978-981-33-6525-4Published: 02 March 2021
Softcover ISBN: 978-981-33-6528-5Published: 03 March 2022
eBook ISBN: 978-981-33-6526-1Published: 01 March 2021
Series ISSN: 1869-1730
Series E-ISSN: 1869-1749
Edition Number: 1
Number of Pages: XIV, 247
Number of Illustrations: 60 b/w illustrations, 89 illustrations in colour
Topics: Aerospace Technology and Astronautics, Thermodynamics, Engineering Fluid Dynamics