Loading...
Please wait, while we are loading the content...
Shock wave-turbulent boundary layer interactions in transonic flow
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Adamson Jr., T. C. Messiter, A. F. |
| Copyright Year | 1976 |
| Description | The method of matched asymptotic expansions is used in analyzing the structure of the interaction region formed when a shock wave impinges on a turbulent flat plate boundary layer in transonic flow. Solutions in outer regions, governed by inviscid flow equations, lead to relations for the wall pressure distribution. Solutions in the inner regions, governed by equations in which Reynolds and/or viscous stresses are included, lead to a relation for the wall shear stress. Solutions for the wall pressure distribution are reviewed for both oblique and normal incoming shock waves. Solutions for the wall shear stress are discussed. |
| File Size | 490276 |
| Page Count | 11 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770003415 |
| Archival Resource Key | ark:/13960/t4dn8xh03 |
| Language | English |
| Publisher Date | 1976-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Shock Waves Flow Equations Transonic Flow Reynolds Number Turbulent Boundary Layer Shear Stress Pressure Distribution Inviscid Flow Separated Flow Asymptotic Methods Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
