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机译:涡流发生器对跨音速后掠翼的影响
Japan Aerosp Explorat Agcy, Aeronaut Technol Directorate, 6-13-1 Osawa, Mitaka, Tokyo 1810015, Japan|AIAA, Reston, VA 20191 USA;
Japan Aerosp Explorat Agcy, Aeronaut Technol Directorate, 6-13-1 Osawa, Mitaka, Tokyo 1810015, Japan|AIAA, Reston, VA 20191 USA;
Japan Aerosp Explorat Agcy, Aeronaut Technol Directorate, 7-44-1 Jindaiji Higashi Machi, Chofu, Tokyo 1828522, Japan;
Japan Aerosp Explorat Agcy, Aeronaut Technol Directorate, 7-44-1 Jindaiji Higashi Machi, Chofu, Tokyo 1828522, Japan|AIAA, Reston, VA 20191 USA;
Japan Aerosp Explorat Agcy, Aeronaut Technol Directorate, 7-44-1 Jindaiji Higashi Machi, Chofu, Tokyo 1828522, Japan|AIAA, Reston, VA 20191 USA;
Japan Aerosp Explorat Agcy, Aeronaut Technol Directorate, 6-13-1 Osawa, Mitaka, Tokyo 1810015, Japan|AIAA, Reston, VA 20191 USA;
Ryoyu Syst Co Ltd, Engn Solut Div, Minato Ku, 2-19-13 Takanawa, Tokyo 1080074, Japan;
机译:跨音速后掠翼上涡流发生器的多点设计优化
机译:通过基于表面的诱集涡流发生器改进固定翼和旋翼跨音速空气动力学
机译:跨音速机翼上涡流发生器分离控制的研究
机译:涡流发生器对跨音速扫频机翼的影响
机译:横掠机翼的跨音速流动:再探冯·卡曼的相似性规则。
机译:快翼形三角翼的前沿旋涡
机译:使用涡流发生器控制高掠过机翼的后缘分离