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  1. コンテンツタイプ
  2. 紀要論文 (Departmental Bulletin Paper)
  1. 機関資料(JAXA, former ISAS, NAL, NASDA)
  2. 旧機関資料 (JAXA, former-ISAS, NAL, NASDA)
  3. 宇宙科学研究所: ISAS Report等を含む (former ISAS (The Institute of Space and Astronautical Science): Including ISAS Report etc.)
  4. ISAS report/Institute of Space and Aeronautical Science,University of Tokyo

A New Running Test Facility for the Study of Flight Dynamics

https://jaxa.repo.nii.ac.jp/records/34416
https://jaxa.repo.nii.ac.jp/records/34416
7a3a417b-95d6-4dfb-bd4f-91eaecbe1839
名前 / ファイル ライセンス アクション
SA2400629.pdf SA2400629.pdf (3.9 MB)
Item type 紀要論文 / Departmental Bulletin Paper(1)
公開日 2015-03-26
タイトル
タイトル A New Running Test Facility for the Study of Flight Dynamics
言語 en
言語
言語 eng
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_6501
資源タイプ departmental bulletin paper
著者 AZUMA, Akira

× AZUMA, Akira

en AZUMA, Akira

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TOMITA, Bunji

× TOMITA, Bunji

en TOMITA, Bunji

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IUCHI, Matsusaburo

× IUCHI, Matsusaburo

en IUCHI, Matsusaburo

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ISHII, Masahiko

× ISHII, Masahiko

en ISHII, Masahiko

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NOGUCHI, Akira

× NOGUCHI, Akira

en NOGUCHI, Akira

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KOJIMA, Tsukasa

× KOJIMA, Tsukasa

en KOJIMA, Tsukasa

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著者所属(英)
en
Uraga Heavy Industry Co., Ltd.
著者所属(英)
en
Uraga Heavy Industry Co., Ltd.
著者所属(英)
en
Uraga Heavy Industry Co., Ltd.
出版者
出版者 東京大学宇宙航空研究所
出版者(英)
出版者 Institute of Space and Aeronautical Science,University of Tokyo
書誌情報 en : ISAS report/Institute of Space and Aeronautical Science,University of Tokyo

巻 34, 号 4, p. 55-73, 発行日 1969-03
抄録(英)
内容記述タイプ Other
内容記述 This is the first part of a report for "A New Running Test Facility for the Study of Flight Dynamics". The facility may be used to evaluate the aerodynamic and/or flight dynamic characteristics of a model of aircraft or, specifically, V/STOL aircraft loaded on a carriage which can move on a track by the maximum speed of ten meters per second. If the model is fixed on the moving carriage low speed aerodynamic characteristics of the model may be obtained by using the internal balance systems installed in the model with similar treatment as well known in the wind tunnel excepting that the model is running instead of flowing the air. If the model is supported on "A New Free Flight System", which can be carried on the carriage, as to be able to fly the model freely for specified directions in any given degrees of freedom, then the flight dynamic characteristics of the model may be evaluated by analyzing the data of the model trajectory which are recorded during the test run. The present report includes the detailed description of the design philosophy, simple explanation of the structural outline and arrangement of the equipments, and the test results for the mechanical performance of the facility.
ISSN
収録物識別子タイプ ISSN
収録物識別子 0372-1418
書誌レコードID
収録物識別子タイプ NCID
収録物識別子 AA00675986
資料番号
内容記述タイプ Other
内容記述 資料番号: SA2400629000
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