2024-06-12T16:16:53Z
https://nagoya.repo.nii.ac.jp/oai
oai:nagoya.repo.nii.ac.jp:00031197
2023-01-16T05:05:47Z
320:2524:2544:2617
An investigation on the interaction between a supersonic boundary layer and a shock wave produced by the wedge slope
Uchida, Shigeo
103078
1970-03-31
A supersonic boundary layer is interacted by the pressure rise produced by a wedge slope. This interaction is found to be similar with the shock wave reflection from the boundary layer. In the present paper the line of displacement thickness is calculated by the momentum integral equation and the outer supersonic flow along this line is obtained by the theory of linearized supersonic flow Matching the outer and the inner flows, we can solve the entire flow field. The principle of calculation and some numerical results are presented.
departmental bulletin paper
Faculty of Engineering, Nagoya University
1970-03-31
Memoirs of the Faculty of Engineering, Nagoya University
2
21
317
330
0027-7657
eng