Loading...
Please wait, while we are loading the content...
Similar Documents
The boundary layer on compressor cascade blades (Document No: 19820008172)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Deutsch, S. |
| Copyright Year | 1981 |
| Description | Some redesign of the cascade facility was necessary in order to incoporate the requirements of the LDA system into the design. Of particular importance was the intended use of a combination of suction upstream of the blade pack with diverging pack walls, as opposed to blade pack suction alone, for spanwise dimensionality control. An ARL blade was used to redo some tests using this arrangement. Preliminary testing and boundary layer measurements began on the double circular arc blades. |
| File Size | 2300440 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820008172 |
| Archival Resource Key | ark:/13960/t79s6kh1z |
| Language | English |
| Publisher Date | 1981-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Static Pressure Cascade Flow Compressor Blades Airfoil Profiles Flow Visualization Pressure Distribution Flow Velocity Inlet Flow Boundary Layers Outlet Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
