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Effect of Inlet-Guide-Vane Angle on Blade Vibration and Rotating Stall of 13-Stage Axial-Flow Compressor in Turbojet Engine
| Author: | Calvert, Howard F. |
|---|---|
| Additional Authors: | Medeiros, Arthur A. |
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E55K03 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61684/ |
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