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Sound wave shear wave interaction with oblique shock fronts final report, 1 sep. 1967 - 31 aug. 1968
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1968 |
| Description | Downstream flow field produced by interaction of plane sound waves or plane shear waves with oblique shock front |
| File Size | 3490250 |
| Page Count | 140 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19690026633 |
| Archival Resource Key | ark:/13960/t6f23q37q |
| Language | English |
| Publisher Date | 1968-08-31 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |