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Bibliographic Record
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- Material Type
- 記事
- Author/Editor
- 濱, 良助HAMA, Ryosuke
- Author Heading
- Publication, Distribution, etc.
- Publication Date
- 1944-12
- Publication Date (W3CDTF)
- 1944-12
- Alternative Title
- The Laminar Boundary Layer in Compressible Fluids with Pressure Gradient.
- Periodical title
- 東京帝國大學航空研究所報告
- No. or year of volume/issue
- 22 321
- Volume
- 22
- Issue
- 321
- Pages
- 451-461
- Text Language Code
- jpn
- Target Audience
- 一般
- Note (General)
- Present paper is concerned with the theory of the laminar boundary layer in compressible fluids. By introducing the stream function φ which is defined by [numerical formula], [numerical formula], the equation of motion [numerical formula] may be transformed into [numerical formula], where x and y are the coordinates along and perpendicular to the wall, and u and v the x and y components of the velocity at any point. Both the density ρ and the viscosity μ are variables, and subscripts 1 and 0 denote the state corresponding to the outer edge of the boundary layer (y→∞) and the standard state corresponding to the state of adiabatic stagnation of the outer flow respectively. When the velocity along the outer edge of the boundary layer is given by u_1=cx^α, the differential equation can be further transformed into [numerical formula], where [numerical formula]. This can be solved by the method of successive approximations as [numerical formula], where [numerical formula], and C is a constant which is to be determined by the boundary condition: u→u_1 as η→∞. This approximation formula may also be described by introducing a nondimensional distance from the wall [numerical formula], then [numerical formula], where [numerical formula], and C is determined as before. Numerical calculations are performed under the conditions such that Prandtl number c_pμ/λ is equal to 1, and heat transfer at the wall is debared. Under these conditions there is a relation between the temperature and the velocity: [numerical formula], and the viscosity is given by [numerical formula] Several numerical results are given in a table and 14 figures.資料番号: SA4148604000
- Access Restrictions
- インターネット公開
- Periodical Title (NCID)
- AA00387631
- Data Provider (Database)
- 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
- Original Data Provider (Database)
- 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ