Applications of Euler equations to sharp edge delta wings with leading edge vorticesStudies on the solution of discrete Euler equations past swept delta wing configurations with sharp leding edges are presented. Freestream Mach numbers range from zero to supersonic, although the Mach number normal to the leading edge is subsonic for all cases discussed. A few examples are given to show the application of the numerical methods to representative problems. The major dicussion is directed at the application of Computational Fluid Dynamics to the understanding of the fundamental fluid mechanic mechanisms of this class of flows.
Document ID
19870010781
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Murman, Earll M. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Rizzi, Arthur (Aeronautical Research Inst. of Sweden Bromma., United States)
Date Acquired
August 13, 2013
Publication Date
November 1, 1986
Publication Information
Publication: AGARD Applications of Computational Fluid Dynamics in Aeronautics