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Dual nozzle aerodynamic and cooling analysis study
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Meagher, G. M. |
| Copyright Year | 1981 |
| Description | Analytical models to predict performance and operating characteristics of dual nozzle concepts were developed and improved. Aerodynamic models are available to define flow characteristics and bleed requirements for both the dual throat and dual expander concepts. Advanced analytical techniques were utilized to provide quantitative estimates of the bleed flow, boundary layer, and shock effects within dual nozzle engines. Thermal analyses were performed to define cooling requirements for baseline configurations, and special studies of unique dual nozzle cooling problems defined feasible means of achieving adequate cooling. |
| File Size | 5480879 |
| Page Count | 264 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810011647 |
| Archival Resource Key | ark:/13960/t43r5pk5m |
| Language | English |
| Publisher Date | 1981-02-27 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Nozzle Design Throats Cooling Aerodynamic Configurations Nozzle Flow Pressure Reduction Flow Characteristics Aerodynamics Boundary Layer Control Dual Thrust Nozzles Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |