Hiroshi Yamashita

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PUBLICATIONS/PRESENTATIONS

    Articles in Journals

  1. Yamashita, H., and Obayashi, S., "Variability of Sonic Boom Intensity and Propagation Path Due to Homogeneous Atmospheric Turbulence," Journal of Aircraft (Under Review).
  2. Yamashita, H., Obayashi, S., and Kusunose, K., "Reduction of Drag Penalty by means of Plain Flaps in Boomless Busemann Biplane," International Journal of Emerging Multidisciplinary Fluid Sciences (Under Review).
  3. Kusunose, K., Matsushima, K., Goto, Y., Maruyama, D., Yamashita, H., and Yonezawa, M., "A Study in the Supersonic Biplane Utilizing its Shock Wave Cancellation Effect," Journal of the Japan Society for Aeronautical and Sciences, Vol.55. No.636, pp.1-7, 2007 (in Japanese).
  4. Yamashita, H., Yonezawa, M., Goto, Y., Obayashi, S., and Kusunose, K., "CFD Analyses of Shock Wave Behavior of Busemann's Biplane," JAXA Special Publication SP-05-017, pp.126-131, 2006 (in Japanese).

    5. Published Contributions to Conferences

  5. Yamashita, H., and Obayashi, S., "Numerical Investigation on Sonic Boom Reduction with Non-axisymmetric Body Shapes," AIAA Paper 2008-0059, 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA, Jan. 2008.
  6. Yamashita, H., Yonezawa, M., and Obayashi, S., "Numerical Study on the Asymmetric Propagation of Near-field Pressure Waves for Sonic Boom Reduction," The Fourth International Conference on Flow Dynamics, Sendai, Japan, Sep. 2007, p.3-4-3.
  7. Kuratani, N., Ogawa, T., Yamashita, H., Yonezawa, M., and Obayashi, S., "Experimental and Computational Fluid Dynamics around Supersonic Biplane for Sonic-Boom Reduction," AIAA Paper 2007-3677, 13th AIAA/CEAS Aeroacoustics Conference, Rome, Italy May 2007.
  8. Yamashita, H., Yonezawa, M., Obayashi, S., and Kusunose, K., "A Study of Busemann-Type Biplane for Avoiding Choked Flow," AIAA Paper 2007-0688, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA, Jan. 2007. (PDF)
  9. Yamashita, H., Yonezawa, M., Obayashi, S., and Kusunose, K., "An Approach to Avoiding Choked Flow for Supersonic Biplane," The Third International Conference on Flow Dynamics, pp.21-22, Matsushima, Japan, Nov. 2006.
  10. Kusunose, K., Maruyama, D., Matsushima, K., Nakahashi, K., Yamashita, H., Yonezawa, M., and Obayashi S, "Toward Silent Supersonic Transport - A Fundamental Study of Supersonic Biplane (Invited)," 4th Joint Meeting of the Acoustical Society of America and the Acoustical Society of Japan, Volume 120, Issue 5, p.3078, Honolulu, Hawaii, Nov. 2006.
  11. Kusunose, K., Matsushima, K., Goto, Y., Yamashita, H., Yonezawa, M., Maruyama, D., and Nakano, T., "A Fundamental Study for the Development of Boomless Supersonic Transport Aircraft," AIAA Paper 2006-0654, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA, Jan. 2006.
  12. Yamashita, H., Yonezawa, M., Goto, Y., Obayashi, S., and Kusunose, K., "CFD Analysis of Shock Waves for Busemann's Biplane," The Second International Conference on Flow Dynamics, p.7-4, Sendai, Japan, Nov. 2005.

    13. Published book

  13. Kusunose, K., Matsushima, K., Obayashi, S., Furukawa, T., Kuratani, N., Goto, Y., Maruyama, D., Yamashita, H., and Yonezawa, M., Aerodynamics Design of Supersonic biplane: Cutting Edge and Related, Tohoku University Press, Sendai, Japan, 2007.

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