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Performance of an inlet having a variable-angle two-dimensional compression surface and a fixed-geometry subsonic diffuser for application to reduced engine rotative speeds- mach numbers 0.66, 1.5, 1.7, and 2.0
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1958 |
| Description | Air inlet for turbojet engines having variable angle two-dimensional compression surface and fixed-geometry subsonic diffuser |
| File Size | 2821096 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630003996 |
| Archival Resource Key | ark:/13960/t6h17rc04 |
| Language | English |
| Publisher Date | 1958-01-30 |
| Access Restriction | Open |
| Subject Keyword | Turbojet Engine 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 |