Loading...
Please wait, while we are loading the content...
Similar Documents
Flow processes in overexpanded chemical rocket nozzles. part 3: methods for the aimed flow separation and side load reduction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Schmucker, R. H. |
| Copyright Year | 1983 |
| Description | Methods aimed at reduction of overexpansion and side load resulting from asymmetric flow separation for rocket nozzles with a high opening ratio are described. The methods employ additional measures for nozzles with a fixed opening ratio. The flow separation can be controlled by several types of nozzle inserts, the properties of which are discussed. Side loads and overexpansion can be reduced by adapting the shape of the nozzle and taking other additional measures for controlled separation of the boundary layer, such as trip wires. |
| File Size | 1034530 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830022246 |
| Archival Resource Key | ark:/13960/t6k11x51b |
| Language | English |
| Publisher Date | 1983-03-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Rocket Nozzles Nozzle Geometry Nozzle Walls Nozzle Flow Nozzle Inserts Grooves Separated Flow Boundary Layers Loads Forces Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
