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Vertical Profiles for Turbojet-Powered AircraftOPTIM 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.
Document ID
19820000312
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Sorensen, J. A. (Analytical Mechanics Associates, Inc.)
Waters, M. H. (Analytical Mechanics Associates, Inc.)
Date Acquired
August 10, 2013
Publication Date
May 1, 1983
Publication Information
Publication: NASA Tech Briefs
Volume: 7
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12940
Accession Number
82B10312
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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