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Computational fluid dynamics - The coming revolutionThe development of aerodynamic theory is traced from the days of Aristotle to the present, with the next stage in computational fluid dynamics dependent on superspeed computers for flow calculations. Additional attention is given to the history of numerical methods inherent in writing computer codes applicable to viscous and inviscid analyses for complex configurations. The advent of the superconducting Josephson junction is noted to place configurational demands on computer design to avoid limitations imposed by the speed of light, and a Japanese projection of a computer capable of several hundred billion operations/sec is mentioned. The NASA Numerical Aerodynamic Simulator is described, showing capabilities of a billion operations/sec with a memory of 240 million words using existing technology. Near-term advances in fluid dynamics are discussed.
Document ID
19820042831
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Graves, R. A., Jr.
(NASA Headquarters Washington, DC United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1982
Publication Information
Publication: Astronautics and Aeronautics
Volume: 20
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
82A26366
Distribution Limits
Public
Copyright
Other

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