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An experimental investigation of the effect of surface heating on boundary-layer transition on a flat plate in supersonic flow
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1951 |
| File Size | 1124188 |
| Page Count | 30 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930083026 |
| Archival Resource Key | ark:/13960/t3vt6092x |
| Language | English |
| Publisher Date | 1951-04-01 |
| Access Restriction | Open |
| Subject Keyword | Reynolds Number Plates, Flat - Temperatures Supersonic Boundary Layer - Plates, Flat Aerodynamics WITH Heat Flow, Laminar Skin Friction Wind Tunnel Tests - Aal - Heat Transfer, Supersonic (6 Inches) Flow, Turbulent Boundary Layer Transition - Plates, Flat Flow - Plates, Flat Boundary Layer - Velocity Distribution 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 |