National Aerospace Laboratory Aerodynamics Division
National Aerospace Laboratory Aerodynamics Division
National Aerospace Laboratory Aerodynamics Division
National Aerospace Laboratory Aerodynamics Division
出版者
航空宇宙技術研究所
出版者（英）
National Aerospace Laboratory (NAL)
雑誌名
航空宇宙技術研究所特別資料
雑誌名(英)
Special Publication of National Aerospace Laboratory
巻
30
ページ
211 - 216
発行年
1996-01
会議概要（会議名, 開催地, 会期, 主催者等）
航空宇宙技術研究所 7-9 Jun. 1995 東京 日本
会議概要（会議名, 開催地, 会期, 主催者等）（英）
National Aerospace Laboratory 7-9 Jun. 1995 Tokyo Japan
A Computational Fluid Dynamics (CFD) code of spectral method of compressible Navier-Stokes equations for the calculation of hypersonic flow around a hemisphere had been developed. An experiment of aerodynamic heating on a series of hemispheres with different diameters had also been accomplished. In this paper, the results between the CFD code, the experiment and the theories are compared, showing that good agreement is obtained.
極超音速流による球の空力加熱の計算と実験との比較
nalsp0030037.pdf
(362.11KB)
