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7. Mechanisms of drag reduction due to flow control around circular disk using coaxial type dielectric barrier discharge plasma actuator at low Reynolds numbers.

12. マッハ5クラスの極超音速実験機の風洞試験

18. 航空・基盤技術と社会に関する懇談会報告 平成18年度:JAXA航空プログラムのあり方と基盤技術の試論

19. A study of three-dimensional interaction flow fields between swept shock waves and turbulent boundary layers: Flow structures and effects of bleed

20. Consideration of Aerodynamic Shape of Hypersonic Turbojet Experimental Vehicle

22. Report of Advisory Group for the Social Relationship on the Aeronautics and Basic Technology in JAXA: Concern on problems of the Aeronautics and its fundamentals for the Nation and JAXA

28. Evaluation of the effects of temperature distortion on the compressor of small pre-cooled turbojet engine

29. Wind tunnel tests and evaluation of aerodynamic performance of experimental airplane with hypersonic engine

30. Report of Advisory Group for the Social Relationship on the Aeronautics and Basic Technology in JAXA: Concern for JAXA's Aviation Program Group with basic research directorate

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