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Propeller aircraft interior noise model
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Wilby, J. F. Pope, L. D. Wilby, E. G. |
| Copyright Year | 1984 |
| Description | An analytical model was developed to predict the interior noise of propeller-driven aircraft. The fuselage model is that of a cylinder with a structurally-integral floor. The cabin sidewall is stiffened by stringers and ring frames, and the floor by longitudinal beams. The cabin interior is covered with a sidewall treatments consisting of layers of porous material and an impervious trim septum. Representation of the propeller pressure field is utilized as input data in the form of the propeller noise signature at a series of locations on a grid over the fuselage structure. Results obtained from the analytical model are compared with test data measured by NASA in a scale model cylindrical fuselage excited by a model propeller. |
| File Size | 4737661 |
| Page Count | 169 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840021618 |
| Archival Resource Key | ark:/13960/t2s51h76t |
| Language | English |
| Publisher Date | 1984-07-01 |
| Access Restriction | Open |
| Subject Keyword | Acoustics Propellers Scale Models Noise Reduction Aircraft Noise Aircraft Compartments Pressure Distribution Signatures Prediction Analysis Techniques Computer Programs 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 |
