Fleming, G. G., Senzig, D. A., McCurdy, D. A., Roof, C. J., & Rapoza, A. S. (2003). Engine installation effects of four civil transport airplanes : Wallops Flight Facility study (Report No. NASA/TM-2003-212433). United States. National Aeronautics and Space Administration. https://rosap.ntl.bts.gov/view/dot/9817
Fleming, Gregg G., David A. Senzig, David A. McCurdy, Christopher J. Roof, and Amanda S. Rapoza. Engine installation effects of four civil transport airplanes : Wallops Flight Facility study. Report no. NASA/TM-2003-212433. United States. National Aeronautics and Space Administration, 2003. https://rosap.ntl.bts.gov/view/dot/9817.
Fleming, Gregg G., et al. Engine installation effects of four civil transport airplanes : Wallops Flight Facility study. United States. National Aeronautics and Space Administration, 2003, Report no. NASA/TM-2003-212433, ROSA P. https://rosap.ntl.bts.gov/view/dot/9817.
This report examines the effects of airplane geometrical configuration on the acoustic directivity characteristics and on the propagation of airplane noise. This effect of airplane geometry is referred to in this report as “engine installation effects.” Engine installation effects are one of the components of lateral attenuation. Lateral attenuation in the Federal Aviation Administration’s (FAA) Integrated Noise Model (INM) has been based on the methods
;
described in the Society of Automotive Engineers’ (SAE) Aerospace Information Report (AIR) 1751. Released in 1981, SAE-AIR-1751 is founded on data measured in the 1960s and 1970s. The Boeing B-727 airplane, which has an engine location not used on more modern large civil transports, dominated these measurements. Long-term measurements conducted with airport noise monitoring equipment have shown that the lateral attenuation algorithms in SAE-AIR-1751 tend to predict too much attenuation for modern airplanes.
Fleming, G. G., Senzig, D. A., McCurdy, D. A., Roof, C. J., & Rapoza, A. S. (2003). Engine installation effects of four civil transport airplanes : Wallops Flight Facility study (Report No. NASA/TM-2003-212433). United States. National Aeronautics and Space Administration. https://rosap.ntl.bts.gov/view/dot/9817
Fleming, Gregg G., David A. Senzig, David A. McCurdy, Christopher J. Roof, and Amanda S. Rapoza. Engine installation effects of four civil transport airplanes : Wallops Flight Facility study. Report no. NASA/TM-2003-212433. United States. National Aeronautics and Space Administration, 2003. https://rosap.ntl.bts.gov/view/dot/9817.
Fleming, Gregg G., et al. Engine installation effects of four civil transport airplanes : Wallops Flight Facility study. United States. National Aeronautics and Space Administration, 2003, Report no. NASA/TM-2003-212433, ROSA P. https://rosap.ntl.bts.gov/view/dot/9817.
ROSA P serves as an archival repository of USDOT-published products including scientific
findings, journal articles, guidelines, recommendations, or other information authored or co-authored by
USDOT or funded partners. As a repository, ROSA P retains documents in their original published format to
ensure public access to scientific information.
Links with this icon indicate that you are leaving a Bureau of Transportation
Statistics (BTS)/National Transportation Library (NTL)
Web-based service.
Thank you for visiting.
You are about to access a non-government link outside of
the U.S. Department of Transportation's National
Transportation Library.
Please note: While links to Web sites outside of DOT are
offered for your convenience, when you exit DOT Web sites,
Federal privacy policy and Section 508 of the Rehabilitation
Act (accessibility requirements) no longer apply. In
addition, DOT does not attest to the accuracy, relevance,
timeliness or completeness of information provided by linked
sites. Linking to a Web site does not constitute an
endorsement by DOT of the sponsors of the site or the
products presented on the site. For more information, please
view DOT's Web site linking policy.
To get back to the page you were previously viewing, click
your Cancel button.