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Flow separation ahead of blunt bodies at supersonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1951 |
| File Size | 19438056 |
| Page Count | 42 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930083006 |
| Archival Resource Key | ark:/13960/t76t50t2g |
| Language | English |
| Publisher Date | 1951-07-01 |
| Access Restriction | Open |
| Subject Keyword | Boundary Layer - Bodies Inlets, Supersonic Flow - Wakes Boundary Layer - Plates Protuberances Bodies - Shape Wind Tunnel Tests - Lfpl - Supersonic (18 Inches X 18 Inches) Boundary Layer - Shock Wave Interaction Flow - Bodies Supersonic 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 |