Nearfield Unsteady Pressures at Cruise Mach Numbers for a Model Scale Counter-Rotation Open Rotor
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An open rotor experiment was conducted at cruise Mach numbers and the unsteady pressure in the nearfield was measured. The system included extensive performance measurements, which can help provide insight into the noise generating mechanisms in the absence of flow measurements. A set of data acquired at a constant blade pitch angle but various rotor speeds was examined. The tone levels generated by the front and rear rotor were found to be nearly equal when the thrust was evenly balanced between rotors. Stephens, David B. Glenn Research Center NASA/TM-2012-217672, E-18347, AIAA Paper 2012-2264
| Publisher Name | Independently Published |
|---|---|
| Author Name | Hagendorf, Col |
| Format | Audio |
| Bisac Subject Major | SCI |
| Language | NG |
| Isbn 10 | 179438149X |
| Isbn 13 | 9781794381490 |
| Target Age Group | min:NA, max:NA |
| Dimensions | 01.10" H x 00.08" L x 50.00" W |
| Page Count | 34 |
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