File
Title Transcription
ワクセイ タイキ トツニュウ ヒコウ ニ トモナウ ゴクチョウオンソク プラズマリュウ ニ カンスル ケンキュウ
Title Alternative
Study on Hypersonic Plasma Flows associated with Planetary Entry Flights
Authors
Keywords
Planetary entry flight
CO2-N2 plasma
Shock tube
Spectroscopy
Nonequilibrium thermochemistry
Abstract
This paper introduces the study on hypersonic plasma flows associated with planetary entry flights. The study is aiming at improving the prediction accuracy of planetary entry flight environments by investigating the characteristics of hypersonic plasma flows behind shock waves generated in entry flight conditions. In the first part of this paper, one of the ground testing facility to simulate entry flight conditions is described. Then, a measurement technique for hypersonic plasma flows is described by introducing the measurement system developed at the test section of a shock tube. After that, spectroscopic data of CO2-N2 plasma flows in an entry flight condition are shown to describe the thermochemical state in the plasma flows. Finally, the summary of this paper is presented.
Publisher
鳥取大学大学院工学研究科
Content Type
Departmental Bulletin Paper
ISSN・ISBN
0385-8596
Journal Title
鳥取大学大学院工学研究科/工学部研究報告
Current Journal Title
鳥取大学大学院工学研究科/工学部研究報告
Volume
45
Start Page
32
End Page
37
Published Date
2014-12-25
Text Version
Publisher
Citation
鳥取大学大学院工学研究科/工学部研究報告. 2014, 45, 32-37
Department
Faculty of Engineering/Graduate School of Engineering
Language
Japanese