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Expansion Waves: Prandtl–Meyer Flow
| Content Provider | Scilit |
|---|---|
| Author | Oosthuizen, Patrick H. Carscallen, William E. |
| Copyright Year | 2013 |
| Description | The discussion given in Chapters 5 and 6 was concerned with waves that involved an increase in pressure, i.e., with shock waves. In this chapter, attention will be given to the types of waves that are generated when there is a decrease in pressure. For example, the type of wave that is generated when a supersonic flow passes over a convex corner and the type of wave that is generated when the end of a duct containing a gas at a pressure that is higher than that in the surrounding air is suddenly opened will be discussed in this chapter. These two situations are illustrated in Figure 7.1. Book Name: Introduction to Compressible Fluid Flow |
| Related Links | https://content.taylorfrancis.com/books/download?dac=C2011-0-04015-9&isbn=9780429109843&doi=10.1201/b15414-12&format=pdf |
| Ending Page | 231 |
| Page Count | 40 |
| Starting Page | 192 |
| DOI | 10.1201/b15414-12 |
| Language | English |
| Publisher | Informa UK Limited |
| Publisher Date | 2013-07-22 |
| Access Restriction | Open |
| Subject Keyword | Book Name: Introduction To Compressible Fluid Flow Convex Corner Prandtl Illustrated Passes |
| Content Type | Text |
| Resource Type | Chapter |
