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The use of a luminescent lacquer for the visual indication of boundary-layer transition
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1951 |
| File Size | 2249473 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082928 |
| Archival Resource Key | ark:/13960/t8pc7b68b |
| Language | English |
| Publisher Date | 1951-01-01 |
| Access Restriction | Open |
| Subject Keyword | Air Flow - Visualization Wind Tunnel Tests - Aal - Heat Transfer, Supersonic (6 Inches) Boundary Layer Transition Wind Tunnel Tests - Aal - Supersonic (3 Feet X 1 Foot) Lacquers 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 |