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NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results
| Content Provider | HathiTrust Digital Library |
|---|---|
| Author | Schulze, Wallace M Ashby, George C Erwin, John R |
| Organization | United States. National Adviosry Committee for Aeronautics. |
| Description | A typical axial-flow compressor rotor using NACA 65-series compressor blades was tested at low speeds and its performance was measured over a range of quantity flow rates at several values of annulus-area ratio, blade-setting angle, solidity, and Reynolds number to compare with porouswall cascade results. The data obtained using varying annulus area were corrected to the two-dimensional-flow condition by two methods Wallace M. Schultze, John R. Erwin, and George C. Ashby, Jr |
| Volume Number | L52L17 |
| Language | English |
| Publisher | National Advisory Committee for Aeronautics |
| Publisher Date | 1953-01-01 |
| Publisher Place | Washington D.C. |
| Access Restriction | Open |
| Rights License | Items in this record are available as Public Domain, Google-digitized. View the access and use profile at http://www.hathitrust.org/access_use#pd-google. Please see individual items for rights and use statements |
| Subject Keyword | Reynolds number Compressors Cascades (Fluid dynamics) Axial flow compressors |
| Content Type | Text |
| Resource Type | Book |
