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OPDOT: A computer program for the optimum preliminary design of a transport airplaneA description of a computer program, OPDOT, for the optimal preliminary design of transport aircraft is given. OPDOT utilizes constrained parameter optimization to minimize a performance index (e.g., direct operating cost per block hour) while satisfying operating constraints. The approach in OPDOT uses geometric descriptors as independent design variables. The independent design variables are systematically iterated to find the optimum design. The technical development of the program is provided and a program listing with sample input and output are utilized to illustrate its use in preliminary design. It is not meant to be a user's guide, but rather a description of a useful design tool developed for studying the application of new technologies to transport airplanes.
Document ID
19830002844
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Sliwa, S. M.
(NASA Langley Research Center Hampton, VA, United States)
Arbuckle, P. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1980
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:81857
NASA-TM-81857
Accession Number
83N11114
Funding Number(s)
PROJECT: RTOP 505-34-33-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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