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Nasa lewis 10 by 10 foot supersonic wind tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Aiello, R. A. |
| Copyright Year | 1974 |
| Description | Performance data are presented for this tunnel, which has a Mach number range from 2.0 to 3.5. The tunnel circuit, model support systems, auxiliary systems, instrumentation, control room equipment, and automatic recording and computing equipment are described. Information is presented on criteria for designing models, and on shop facilities available to users. |
| File Size | 1382919 |
| Page Count | 47 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750006708 |
| Archival Resource Key | ark:/13960/t8qc4sq6n |
| Language | English |
| Publisher Date | 1974-11-01 |
| Access Restriction | Open |
| Subject Keyword | Research And Support Facilities (air) Aerodynamics Test Facilities Aeronautical Engineering Test Equipment Supersonic Wind Tunnels Measuring Instruments Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |