@inproceedings{oai:jaxa.repo.nii.ac.jp:00047325,
 author = {藤尾, 秩寛 and 小川, 秀朗 and FUJIO, Chihiro and OGAWA, Hideaki},
 book = {宇宙航空研究開発機構特別資料: 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オンライン論文集, JAXA Special Publication: Proceedings of Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online},
 month = {Feb},
 note = {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},
 pages = {27--36},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {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},
 volume = {JAXA-SP-20-008},
 year = {2021}
}