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Evaluation of the Advanced Subsonic Technology Program Noise Reduction BenefitsThis report presents a detailed evaluation of the aircraft noise reduction technology concepts developed during the course of the NASA/FAA Advanced Subsonic Technology (AST) Noise Reduction Program. In 1992, NASA and the FAA initiated a cosponsored, multi-year program with the U.S. aircraft industry focused on achieving significant advances in aircraft noise reduction. The program achieved success through a systematic development and validation of noise reduction technology. Using the NASA Aircraft Noise Prediction Program, the noise reduction benefit of the technologies that reached a NASA technology readiness level of 5 or 6 were applied to each of four classes of aircraft which included a large four engine aircraft, a large twin engine aircraft, a small twin engine aircraft and a business jet. Total aircraft noise reductions resulting from the implementation of the appropriate technologies for each class of aircraft are presented and compared to the AST program goals.
Document ID
20050186548
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Golub, Robert A.
(NASA Langley Research Center Hampton, VA, United States)
Rawls, John W., Jr.
(Lockheed Martin Engineering and Science Services Hampton, VA, United States)
Russell, James W.
(Lockheed Martin Engineering and Science Services Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 2005
Subject Category
Acoustics
Report/Patent Number
NASA/TM-2005-212144
L-19050
Report Number: NASA/TM-2005-212144
Report Number: L-19050
Funding Number(s)
OTHER: 23-781-20-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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