Mixed Transonic Flow over a Wavy Wall with Embedded Shock Waves
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | CHANG, Keun-Shik | - |
| dc.contributor.author | KWON, O. J. | - |
| dc.date.accessioned | 2011-09-22T08:36:26Z | - |
| dc.date.available | 2011-09-22T08:36:26Z | - |
| dc.date.issued | 1983 | - |
| dc.identifier.citation | Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 25, No.70, pp. 189-202. | en |
| dc.identifier.issn | 0549-3811 | - |
| dc.identifier.uri | http://hdl.handle.net/10203/25276 | - |
| dc.description.abstract | Transonic potential flow over an infinitely-long plane wall corrugated in the form of a streamwise sinusoidal wave has been solved using Murman's finite difference scheme based on small perturbation theory. The range of a transonic similarity parameter, K, is determined in which a subsonic/supersonic mixed flow exist. The structure of the mixed flow is studied in detail for various supercritical free stream Mach numbers. By investigating the transitional transonic drag-rising phenomenon it is found that wave drag is negligibly small in the supercritical parameter range 5.7 ≤ K ≤ 7.02, due to the near-symmetry of locally supersonic flow about the crest of the wavy wall. | en |
| dc.language.iso | en_US | en |
| dc.publisher | The Japan Society for Aeronautical and Space Sciences | en |
| dc.title | Mixed Transonic Flow over a Wavy Wall with Embedded Shock Waves | en |
| dc.type | Article | en |
- Appears in Collection
- AE-Journal Papers(저널논문)
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