VSRA/DLCフラップ系の安定・操縦微係数の同定

Material type: 文書・図像類

Author: 塚野, 雄吉ほか

Publisher: 航空宇宙技術研究所

Publication date: 1991-07

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: DLCフラップを装着した可変安定応答実験機(VSRA)のシステム・パラメータを知るために強制振動法による飛行実験を行った。水平定常飛行状態のトリムまわりで,DLCフラップを種々の周波数で持続的に加振し,その機体応答の周波数特性データからVSRAシステムの安定・操縦微係数を同定した。さらに,その操縦微...

Search by Bookstore

Holdings of Libraries in Japan

This page shows libraries in Japan other than the National Diet Library that hold the material.

List of Cooperating Institutions and Databases

Please contact your local library for information on how to use materials or whether it is possible to request materials from the holding libraries.

other

JAXA Repository
Digital
You can check the holdings of institutions and databases with which Institutional Repositories DataBase(IRDB)(Institutional Repository) is linked at the site of Institutional Repositories DataBase(IRDB)(Institutional Repository).
JAXA Repository

Search by Bookstore

Bibliographic Record

You can check the details of this material, its authority (keywords that refer to materials on the same subject, author's name, etc.), etc.

Digital

Material Type: 文書・図像類
Title: VSRA/DLCフラップ系の安定・操縦微係数の同定
Author/Editor: 塚野, 雄吉
小野, 孝次
石川, 和敏
TSUKANO, Yukichi
ONO, Takatsugu
ISHIKAWA, Kazutoshi
Author Heading: 塚野, 雄吉
小野, 孝次
石川, 和敏
TSUKANO, Yukichi
ONO, Takatsugu
ISHIKAWA, Kazutoshi
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1991-07
Publication Date (W3CDTF): 1991-07
Alternative Title: Identification of the Stability and Control Derivatives of a DLC-Flap System for VSRA.
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-1116
No. or year of volume/issue: 1116
Volume: 1116
Pages: 16-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Subject Heading: Stability/Control derivatives; Flight Tests; Frequency Response Method; DLC-flaps; In-flight simulator
Target Audience: 一般
Note (General): DLCフラップを装着した可変安定応答実験機(VSRA)のシステム・パラメータを知るために強制振動法による飛行実験を行った。水平定常飛行状態のトリムまわりで,DLCフラップを種々の周波数で持続的に加振し,その機体応答の周波数特性データからVSRAシステムの安定・操縦微係数を同定した。さらに,その操縦微係数からDLCフラップの揚力,抗力そして縦揺れモーメントを推定し,風洞試験結果とも比較した。その実験方法並びにデータ解析手法について述べる。
Flight tests were conducted using the Variable Stability and Response Airplane (VSRA) in order to identify the stability and control derivatives for a Direct Lift Control (DLC) flap system. The frequency response method was selected, with a pure sinusoidal input being applied to the DLC-flaps. Response from a linear system model consisting of the stability and control derivatives were compared with other flight test response data to determine general-inputs and resulting derivatives were subsequently verified. In addition, the control capability of the DLC-flaps was estimated by the control derivatives, and their compared with wind tunnel test data.
資料番号: NALTR1116000
レポート番号: NAL TR-1116
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