Numerical simulation of the flow field around a complete aircraftThe present effort represents a first attempt of numerical simulation of the flow field around a complete aircraft-like, lifting configuration utilizing the Reynolds averaged Navier-Stokes equations. The numerical solution generated for the experimental aircraft concept X24C-10D at a Mach number of 5.95 not only exhibited accurate prediction of detailed flow properties but also of the integrated aerodynamic coefficients. In addition, the present analysis demonstrated that a page structure of data collected into cyclic blocks is an efficient and viable means for processing the Navier-Stokes equations on the CRAY XMP-22 computer with external memory device.
Document ID
19870010798
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shang, J. S. (Air Force Wright Aeronautical Labs. Wright-Patterson AFB, OH, United States)
Scherr, S. J. (Air Force Wright Aeronautical Labs. Wright-Patterson AFB, OH, United States)
Date Acquired
August 13, 2013
Publication Date
November 1, 1986
Publication Information
Publication: AGARD Applications of Computational Fluid Dynamics in Aeronautics