Prediction and Validation Technologies of Aerodynamic Force and Heat for Hypersonic Vehicle Design

AvMin Zhao

Häftad, Engelska, 2022

Del i serien Springer Aerospace Technology

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Beskrivning

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.

Produktinformation

Utgivningsdatum:2022-03-03
Mått:155 x 235 x 15 mm
Vikt:406 g
Format:Häftad
Språk:Engelska
Serie:Springer Aerospace Technology
Antal sidor:247
Upplaga:22001
Förlag:Springer Verlag, Singapore
ISBN:9789813365285
Originaltitel:GAO CHAO SHENG SU QI DONG LI RE HUAN JING XIN XING YU CE YU YAN ZHENG JI SHU

Utforska kategorier

Flyg- och rymdteknik inom Naturvetenskap och teknik
Fysik inom Naturvetenskap och teknik
Rymdforskning inom Naturvetenskap och teknik

Mer om författaren

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.

Innehållsförteckning

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.