スクラムジェット上昇飛行に向けた流線追跡法によるインテーク設計に関する数値的研究

機関リポジトリ

書誌事項

タイトル別名
  • Parametric Characterization of Streamline Traced Intake Design for Scramjet-Powered Ascent Flight

抄録

流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2020オンライン (2020年9月28日-30日. 日本航空宇宙学会 : 宇宙航空研究開発機構(JAXA)オンライン会議)

Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online (September 28-30, 2020. The Japan Society for Aeronautical and Space Sciences : Japan Aerospace Exploration Agency (JAXA), Online meeting)

Streamline tracing is an effective technique to design efficient and robust three-dimensional intakes for scramjet engines, a hypersonic airbreathing propulsion technology that offers promise for economical and flexible access-to-space. A parametric study has been conducted to classify possible geometries and characterize the relations between design variables and resultant geometries. Computational investigation has been performed for some representative geometries of each class to evaluate the performance and geometries, and to identify key design parameters. The physical insight gained in this study provides a guideline for the usage of the streamline tracing technique for high-performance scramjet intake design.

形態: カラー図版あり

Physical characteristics: Original contains color illustrations

資料番号: AA2030013004

レポート番号: JAXA-SP-20-008

収録刊行物

詳細情報 詳細情報について

  • CRID
    1050855511199765504
  • NII論文ID
    120006954838
  • ISSN
    24332232
  • Web Site
    http://id.nii.ac.jp/1696/00047312/
  • 本文言語コード
    ja
  • 資料種別
    conference paper
  • データソース種別
    • IRDB
    • CiNii Articles

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