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F100 exhaust nozzle area control
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kozlin, J. R. |
| Copyright Year | 1980 |
| Description | The details of the F100 nozzle mechanism design are highlighted, placing particular emphasis upon the evolution of design constraints or drivers from initial concept through current operational deployment. A kinematic description of the area control mechanism is given, and several environmental constraints which complicate the normal mechanism design process are discussed. |
| File Size | 1060526 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800015022 |
| Archival Resource Key | ark:/13960/t9g49hf5v |
| Language | English |
| Publisher Date | 1980-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Nozzle Design Aerodynamic Configurations Exhaust Nozzles Flow Distribution Convergent-divergent Nozzles Turbofan Engines Static Loads F-100 Aircraft Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |