Development of a Detonation Driver for a Shock Tunnel

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The need for high enthalpy facilities for simulating the atmospheric entry of bodies has required the development of hypervelocity wind tunnels. From the various possibilities to produce stagnation enthalpies in the range up to 20 MJ/kg the shock tunnels still are very attractive. The required high temperature driver is accomplished in the present work by a oxyhydrogen detonation in the driver section of the shock tunnel. To study the performance range of such a driver type we investigated the behaviour of a detonation driven shock tube. The experimental research aimed at the improvement of the diaphragms, the history of pressures and the structural stresses.

収録刊行物

  • 高圧力の科学と技術 = The Review of high pressure science and technology  

    高圧力の科学と技術 = The Review of high pressure science and technology 7, 879-884, 1998 

    The Japan Society of High Pressure Science and Technology

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各種コード

  • NII論文ID(NAID)
    10002692196
  • NII書誌ID(NCID)
    AN10452913
  • 本文言語コード
    ENG
  • 資料種別
    ART
  • ISSN
    0917639X
  • NDL 記事登録ID
    4494089
  • NDL 雑誌分類
    ZP1(科学技術--化学・化学工業)
  • NDL 請求記号
    Z17-1589
  • データ提供元
    CJP書誌  NDL  J-STAGE 
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