Venkatakrishnan, L and Krothapalli, A (2006) Forward flight effects on fan noise from supersonic 2-D inlets. Journal of Aircraft, 43 (5). pp. 1549-1552. ISSN 0021-8669
Full text available as:![[img]](http://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) | PDF Download (1562Kb) |
Abstract
THE success of high-speed civil transport aircraft depends on the minimization of its environmental impact. Foremost among these is the aircraft community noise due to takeoff and landing. In addition to jet noise, forward-propagated engine fan noise is a significant component of the overall noise. The noise radiation directivity pattern is influenced by the design of the inlet. This is especially13; true for supersonic inlets where features such as translating centerbody, support struts, and auxiliary doors are contributing factors.
| Item Type: | Journal Article |
|---|---|
| Additional Information: | Copyright for this article belongs to AIAA |
| Uncontrolled Keywords: | Noise;Inlets;Aircraft;Aircraft components;Forward flight;Struts;Optimization;Environmental impact;High speed;Communities;Centerbodies;Aerospace engines;Supersonic inlets;Jet noise;Takeoff;Doors;Directivity;Landing;Transport aircraft |
| Subjects: | AERONAUTICS > Aeronautics (General) AERONAUTICS > Aircraft Design, Testing & Performance |
| Division/Department: | Experimental Aerodynamics Division, Other |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 23 Feb 2010 |
| Last Modified: | 07 Jun 2010 15:57 |
| URI: | http://nal-ir.nal.res.in/id/eprint/4309 |
Actions (login required)
| View Item |
