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Laminar flow supersonic wind tunnel primary air injector
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Smith, Brooke Edward |
| Copyright Year | 1993 |
| Description | This paper describes the requirements, design, and prototype testing of the flex-section and hinge seals for the Laminar Flow Supersonic Wind Tunnel Primary Injector. The supersonic atmospheric primary injector operates between Mach 1.8 and Mach 2.2 with mass-flow rates of 62 to 128 lbm/s providing the necessary pressure reduction to operate the tunnel in the desired Reynolds number (Re) range. |
| File Size | 565600 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19940025146 |
| Archival Resource Key | ark:/13960/t0cv9f13h |
| Language | English |
| Publisher Date | 1993-05-01 |
| Access Restriction | Open |
| Subject Keyword | Research And Support Facilities (air) Hinges Seals Stoppers Injectors Centrifugal Compressors Mass Flow Rate Laminar Flow Prototypes Supersonic Wind Tunnels Pressure Reduction Wind Tunnel Apparatus Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |