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Massachusetts Institute of Technology

Design trade studies and assessment for advanced quiet aircraft concepts

Abstract

dc:description.abstract

(cont.) designed for 4,000nm range, 25,000 to 35,000ft cruise altitude, Mach 0.8 at cruise, and 10,000 to 14,000ft takeoff field length. By identifying the main high-level design drivers of an aircraft design, the mission for a baseline silent aircraft planform and engine was determined. A silent aircraft was designed for a range of 4,000nm and 250 passengers. A noise assessment was conducted on the engine and airframe noise sources of the resulting design. The noise impacts of five engine (jet, fan forward, fan rearward, core, and turbine) and airframe (airfoil, elevator, slat, drag rudder, and undercarriage) noise sources were investigated in terms of their noise footprints and, more specically, the loudest noise caused outside the airport boundary. The greatest noise source was the drag rudder, which was required to offset the idle thrust of the engine during approach. Because of the variable cycle and shielding effects on the embedded engines, engine noise at takeoff was greatly reduced. The main contribution of engine noise was the fan rearward noise. Overall, airframe and engine noise during approach was found to be 12dBA and 9dBA louder than during takeoff respectively. The loudest airframe noise occurred during a 3-degree approach, and was about 6dBA louder than engine noise.

Degree

thesis:*
Department dc:contributor.department
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2005

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Tan, David York Luen, 1979-
Advisor dc:contributor.advisor
  • Karen E. Willcox.

Subjects

dc:subject × 1

Rights

dc:rights
Statement dc:rights
  • M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.
Language dc:language.iso
en_US

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/1721.1/27863
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/27863

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Tan, David York Luen, 1979-. Design trade studies and assessment for advanced quiet aircraft concepts. Massachusetts Institute of Technology, 2005. http://hdl.handle.net/1721.1/27863