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  1. B200 工学部/工学研究科
  2. B200a 雑誌掲載論文
  3. 学術雑誌

ANALYSES OF FLOW FIELD STRUCTURES AROUND LINEAR-TYPE AEROSPIKE NOZZLES USING LIF AND PSP

http://hdl.handle.net/2237/7168
http://hdl.handle.net/2237/7168
31a8f121-e53d-4f07-8ba3-c3ee7699286e
名前 / ファイル ライセンス アクション
ICIASF_2003_15.pdf ICIASF_2003_15.pdf (824.4 kB)
Item type 学術雑誌論文 / Journal Article(1)
公開日 2006-12-12
タイトル
タイトル ANALYSES OF FLOW FIELD STRUCTURES AROUND LINEAR-TYPE AEROSPIKE NOZZLES USING LIF AND PSP
言語 en
著者 Niimi, Tomohide

× Niimi, Tomohide

WEKO 14460

en Niimi, Tomohide

Search repository
Mori, Hideo

× Mori, Hideo

WEKO 14461

en Mori, Hideo

Search repository
Okabe, Kazuki

× Okabe, Kazuki

WEKO 14462

en Okabe, Kazuki

Search repository
Masai, Yusuke

× Masai, Yusuke

WEKO 14463

en Masai, Yusuke

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Taniguchi, Mashio

× Taniguchi, Mashio

WEKO 14464

en Taniguchi, Mashio

Search repository
アクセス権
アクセス権 open access
アクセス権URI http://purl.org/coar/access_right/c_abf2
権利
言語 en
権利情報 Copyright © 2003 IEEE. Reprinted from (relevant publication info). This material is posted here with permission of the IEEE. Such permission of the IEEE does not in any way imply IEEE endorsement of any of Nagoya University’s products or services. Internal or personal use of this material is permitted. However, permission to reprint/republish this material for advertising or promotional purposes or for creating new collective works for resale or redistribution must be obtained from the IEEE by writing to pubs-permissions@ieee.org.
抄録
内容記述 Aerospike nozzles have been expected as a candidate for an engine of reusable Space Shuttles to respond to growing demand for rocket-launching at the lower cost. In this study, the flow field structures in any cross sections around the linear-type aerospike nozzle are visualized and analyzed, using laser induced fluorescence (LIF) of NO seeded in the carrier gas N/sub 2/. Since the flow field structure is affected mainly by the pressure ratio (P/sub s//P/sub a/), the linear-type aerospike nozzle is set inside the vacuum chamber to carry out the experiments in the wide range of pressure ratios from 75 to 250. Flow fields are visualized in several cross-sections, demonstrating the complicated three-dimensional flow field structures. Pressure sensitive paint (PSP) of PtTFPP bound by poly(TMSP) is also applied successfully to measurement of the complicated pressure distribution on the spike surface.
言語 en
内容記述タイプ Abstract
出版者
言語 en
出版者 IEEE
言語
言語 eng
資源タイプ
資源タイプresource http://purl.org/coar/resource_type/c_6501
タイプ journal article
出版タイプ
出版タイプ VoR
出版タイプResource http://purl.org/coar/version/c_970fb48d4fbd8a85
DOI
関連タイプ isVersionOf
識別子タイプ DOI
関連識別子 https://doi.org/10.1109/ICIASF.2003.1274847
ISBN
関連タイプ isPartOf
識別子タイプ ISBN
関連識別子 0-7803-8149-1
書誌情報 en : 20th International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF '03)

p. 15-20, 発行日 2003-08
フォーマット
application/pdf
著者版フラグ
値 publisher
URI
識別子 http://hdl.handle.net/2237/7168
識別子タイプ HDL
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