INM. Integrated Noise Model Version 4.11. User's Guide - Supplement


Book Description

The John A. Volpe National Transportation Systems Center (Volpe Center), in support of the Federal Aviation administration, Office of Environment and Energy, has developed Version 4.11 of the Integrated Noise Model (INM). The User's Guide for the Version 4.11 computer software is a supplement to INM, Version 3, User's Guide - Revision 1 for the Version 3.10 computer software released in June, 1992. The Version 4.11 supplement, prepared by the Volpe Center's Acoustics Facility, presents computer system requirements as well as installation procedures and enhancements. Specific enhancements discussed include: (1) the introduction of a takeoff profile generator; (2) the ability to account for terrain elevation around a specified airport; (3) the ability to compute the CNEL, WECPNL, LEQDAY, and LEQNIGHT noise metrics; (4) the ability to account for airplane runup operations; (5) the ability to account for displaced runway thresholds during approach operations; (6) an enhancement to the noise contour computations: (7) an increase in the number of takeoff profile segments; and (8) enhancements to the echo file. Airport noise, Computer Model, Noise Contours, Integrated Noise Model, Noise Level Prediction, FAR Part 150.



















FAA Integrated Noise Model, Version 1


Book Description




INM User's Guide


Book Description




Integrated Noise Model (INM). Version 2. User's Guide


Book Description

This document contains the instructions to execute the Integrated Noise Model (INM), Version 2. The INM is a collection of computer programs which can calculate the aircraft noise environment in the vicinity of an airport given certain information on airport location, layout, and the type and movement of its air traffic.




Review of Integrated Noise Model (Inm) Equations and Processes


Book Description

The FAA's Integrated Noise Model (INM) relies on the methods of the SAE AIR-1845 'Procedure for the Calculation of Airplane Noise in the Vicinity of Airports' issued in 1986. Simplifying assumptions for aerodynamics and noise calculation were made in the SAE standard and the INM based on the limited computing power commonly available then. The key objectives of this study are 1) to test some of those assumptions against Boeing source data, and 2) to automate the manufacturer's methods of data development to enable the maintenance of a consistent INM database over time. These new automated tools were used to generate INM database submissions for six airplane types:737-700 (CFM56-7 24K), 767-400ER (CF6-80C2BF), 777-300 (Trent 892), 717-200 (BR7 15), 757-300 (RR535E4B), and the 737-800 (CFM56-7 26K).Shepherd, Kevin P. (Technical Monitor) and Forsyth, David W. and Gulding, John and DiPardo, JosephLangley Research CenterAIRCRAFT NOISE; NOISE PREDICTION (AIRCRAFT); AIRCRAFT MODELS; AERODYNAMIC NOISE; JET AIRCRAFT; AIRPORTS; EXTRAPOLATION; DATA BASES; WEIGHT (MASS); THRUST DISTRIBUTION