Enhanced AEDT Modeling of Aircraft Arrival and Departure Profiles, Volume 1: Guidance (2018) / Chapter Skim
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Pages 6-10
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Page 6 radius of about 20 miles up to an altitude of 10,000 ft Above Field Elevation (AFE)
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Page 7 Figure 1. Profile Modeling Methods in AEDT and ACRP 02-55 Existing AEDT Methods Originating from INM The standard or default flight profiles available in AEDT were originally developed for the INM.
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Page 8 assigned flight profile. As discussed later in this Guidance Document, FAA approval is required for any user-defined custom profile – a process which can be time and resource intensive.
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Page 9 corrected net thrust, based on TAS and pressure. Flap Coefficients For each flap setting of an airplane, coefficients to determine drag-to-lift ratio, landing CAS, takeoff CAS, and the aerodynamic component of takeoff ground roll length.
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From page 10... ...
Page 10 determined that the use of reduced-thrust settings and potentially increased weight assumptions is helpful in order to obtain reasonable approximations without exceeding speed limits (i.e., the 250 knot constraint)
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