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New broadband shock noise model and computer code for anopp
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Reddy, N. N. |
| Copyright Year | 1992 |
| Description | The basic mechanism for broadband shock noise in supersonic jets is the interaction between the shock waves and the turbulence in the jet exhaust. This source is in addition to jet mixing noise. |
| File Size | 726800 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19940028983 |
| Archival Resource Key | ark:/13960/t81k49z8t |
| Language | English |
| Publisher Date | 1992-04-01 |
| Access Restriction | Open |
| Subject Keyword | Acoustics Supersonic Flow Turbulent Flow Sound Propagation Acoustic Properties Supersonic Speed Shock Wave Propagation Flow Distribution Aerodynamic Noise Jet Exhaust Noise Measurement Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |