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Effect of nozzle lateral spacing on afterbody drag and performance of twin-jet afterbody models with convergent nozzles at mach numbers up to 2.2
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1970 |
| Description | Nozzle lateral spacing effect on drag and performance of twin jet afterbody configurations with convergent nozzles at Mach 0.6 to 2.2 |
| File Size | 14158542 |
| Page Count | 146 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19710000802 |
| Archival Resource Key | ark:/13960/t2n63932g |
| Language | English |
| Publisher Date | 1970-10-01 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems 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 |