| タイトル | Computation of imaginary-side pressure distributions over the flexible walls of the test section insert for the 0.3-M transonic cryogenic tunnel |
| 本文（外部サイト） | http://hdl.handle.net/2060/19840019610 |
| 著者（英） | Goodyer, M. J. |
| 著者所属（英） | Southampton Univ. |
| 発行日 | 1984-06-01 |
| 言語 | eng |
| 内容記述 | Two dimensional airfoil testing in an adaptive wall test-section wind tunnel requires the computation of the imaginary flow fields extending outward from the top and bottom test section walls. A computer program was developed to compute the flow field which would be associated with an arbitrary test section wall shape. The program is based on incompressible flow theory with a Prandtl-Glauert compressibility correction. The program was validated by comparing the streamline and the pressure field generated by a source in uniform flow with the results from the computer program. A listing of the program, the validation test results, and a sample program are included. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 84N27678
NASA-CR-172363
NAS 1.26:172363 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/159155 |
