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An analysis of supersonic aerodynamic heating with continuous fluid injection (Document No: 19930082730)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1949 |
| File Size | 1777981 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082730 |
| Archival Resource Key | ark:/13960/t33248p01 |
| Language | English |
| Publisher Date | 1949-12-01 |
| Access Restriction | Open |
| Subject Keyword | Plates, Flat - Temperatures Cooling Systems, Sweat Heating, Aerodynamic Boundary Layer, Laminar Boundary Layer - Stability Coolants Skin Friciton Heat Transmission - Boundary Layer 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 |