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Transonic propulsion system integration analysis at McDonnell Aircraft CompanyThe technology of Computational Fluid Dynamics (CFD) is becoming an important tool in the development of aircraft propulsion systems. Two of the most valuable features of CFD are: (1) quick acquisition of flow field data; and (2) complete description of flow fields, allowing detailed investigation of interactions. Current analysis methods complement wind tunnel testing in several ways. Herein, the discussion is focused on CFD methods. However, aircraft design studies need data from both CFD and wind tunnel testing. Each approach complements the other.
Document ID
19890011572
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cosner, Raymond R.
(McDonnell Aircraft Co. Saint Louis, MO, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1989
Publication Information
Publication: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 2
Subject Category
Aircraft Propulsion And Power
Accession Number
89N20943
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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