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Comparison of NACA 65-series compressor-blade pressure distributions and performance in a rotor and in cascade
| Content Provider | HathiTrust Digital Library |
|---|---|
| Author | Westphal, Willard R Godwin, William R |
| Editor | Willard R. Westphal William R. Godwin |
| Organization | United States. National Adviosry Committee for Aeronautics. |
| Description | An investigation has been conducted to compare the performance of NACA 65-series compressor blades in two-dimensional cascade with that in an axial-flow compressor. The entering and leaving flow velocities, pressure rise, and the pressure distribution on the rotating blades were measured at three radial stations of a free-vortex rotor. The blade pressure distributions were obtained by the use of a mercury-seal pressure-transfer device. The data obtained were compared with similar data for the same blade sections obtained from a two-dimensional porous-wall cascade tunnel |
| Volume Number | L51H20 |
| Language | English |
| Publisher | National Advisory Committee for Aeronautics |
| Publisher Date | 1951-01-01 |
| 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 | Blades Cascades (Fluid dynamics) Aerodynamic load Compressors Turbomachines |
| Content Type | Text |
| Resource Type | Book |
