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Investigation of an underslung scoop inlet at mach numbers to 1.99 (Document No: 19650018860)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1957 |
| Description | Supersonic wind tunnel test of underslung scoop inlet on body of revolution |
| File Size | 3081457 |
| Page Count | 40 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19650018860 |
| Archival Resource Key | ark:/13960/t7tn1z53c |
| Language | English |
| Publisher Date | 1957-03-13 |
| Access Restriction | Open |
| Subject Keyword | Body OF Revolution Supersonic Wind Tunnel Air Inlet 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 |