NASA NTRS · 19820000312
Vertical Profiles for Turbojet-Powered Aircraft
Abstract
OPTIM generates profile of altitude, airspeed, and flightpath angle as function of range between given set or origin and destination points for particular models of transport aircraft. Profile is optimized in sense of minimizing fuel or time or in minimizing direct operating cost expressed as combination of fuel and time.
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Sorensen, J. A., Waters, M. H.. 1983-05-01. Vertical Profiles for Turbojet-Powered Aircraft. https://ntrs.nasa.gov/citations/19820000312
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