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Effect of blade leading edge thickness on cavitation performance of 80.6 deg helical inducer in hydrogen
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1970 |
| Description | Effect of blade leading edge thickness on cavitation performance of helical inducer in hydrogen |
| File Size | 1282983 |
| Page Count | 24 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19700021516 |
| Archival Resource Key | ark:/13960/t2s51dn5g |
| Language | English |
| Publisher Date | 1970-06-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics 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 |