High Speed and High Angle of Attack Aerodynamic Characteristics of Winged Space Vehicle

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説明

Static aerodynamic characteristics of winged space vehicle is investigated through a series of wind tunnel testing. This report includes a summary of the test results and associated considerations. The tests were conducted and supported by Working Group for Winged Space Vehicle of Institute of Space and Astronautical Science (ISAS). Attention has been concentrated on both longitudinal and lateral/directional, high angle of attack flight capability at high speed flight condition of the vehicle for the accomplishment of the reentry flight, so that three types of tail configuration are investigated, that are single and double-tails and tip-fin configurations. Test results are summarized in terms of aerodynamic coefficients and their derivatives. Discussions based on the test results are made to find out the relations between vehicle configuration and various aerodynamic and flight dynamic characteristics, which refers the high angle of attack flight criteria of current high-performance airplanes.

資料番号: SA0035030000

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詳細情報 詳細情報について

  • CRID
    1050003824960953344
  • NII論文ID
    110000029137
  • NII書誌ID
    AA10632072
  • ISSN
    02856808
  • Web Site
    http://id.nii.ac.jp/1696/00031383/
  • 本文言語コード
    en
  • 資料種別
    departmental bulletin paper
  • データソース種別
    • IRDB
    • CiNii Articles

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