Transonic Operational Characteristics and Performance of Two Turbine-Powered Simulators Determined From Wind Tunnel Tests

Material type: 文書・図像類

Author: 小池, 陽ほか

Publisher: 航空宇宙技術研究所

Publication date: 1988-03

Material Format: Digital

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Note (General)：: Two TPS’s manufactured by Tech Development Inc.(Model 1079A), clad with nacelles of a generic configuration, are subjected to test in the NAL 2m ×2m T...

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Material Type: 文書・図像類
Title: Transonic Operational Characteristics and Performance of Two Turbine-Powered Simulators Determined From Wind Tunnel Tests
Author/Editor: 小池, 陽
浅井, 圭介
細江, 信幸
唐沢, 敏夫
末永, 尚史
三掘, 進
鈴木, 弘一
KOIKE, Akira
ASAI, Keisuke
HOSOE, Nobuyuki
KARASAWA, Toshio
SUENAGA, Hisashi
MITSUBORI, Susumu
SUZUKI, Koichi
Author Heading: 小池, 陽
浅井, 圭介
細江, 信幸
唐沢, 敏夫
末永, 尚史
三掘, 進
鈴木, 弘一
KOIKE, Akira
ASAI, Keisuke
HOSOE, Nobuyuki
KARASAWA, Toshio
SUENAGA, Hisashi
MITSUBORI, Susumu
SUZUKI, Koichi
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1988-03
Publication Date (W3CDTF): 1988-03
Alternative Title: 遷音速におけるTPS特性試験
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-968
No. or year of volume/issue: 968
Volume: 968
Pages: 30-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: eng
Target Audience: 一般
Note (General): Two TPS’s manufactured by Tech Development Inc.(Model 1079A), clad with nacelles of a generic configuration, are subjected to test in the NAL 2m ×2m Transonic Wind Tunnel up to a Mach number of 0.8 in order to obtain data needed for use of the TPS’s in a high-speed wind tunnel test of the NAL STOL research airplane ‘ASKA’. The TPS’s are placed on top of a strut erected on the balance turn-table of the test-section floor so that the aerodynamic forces acting on the nacelle-strut system can be measured. Operational characteristics are obtained by measuring the TPS fan rotational speed as a function of the turbine-drive air pressure, and by observing the variation of the temperatures at the bearings supporting the TPS rotational part. Acceleration levels due to vibration are also measured. Instrumentation includes the total pressure- and temperature distributions within the fan- and turbine nozzle flows to derive the TPS/nacelle performance represented by the fan pressure ratio, the mass flow through the fan and the magnitude of the thrust generated by the TPS/nacelle system.
資料番号: NALTR0968000
レポート番号: NAL TR-968
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ