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Shock diffraction computations over complex structuresThis work contains the results of a study aimed at the development of two- and three-dimensional numerical procedures for computing the flowfield generated by the interaction of a blast wave and a rigid body. A number of numerical procedures were applied to two-dimensional problems including both implicit and explicit algorithms. Each was tried on the blast wave-cylinder interaction problem. MacCormack's (1969) method with added fourth-order dissipation yielded the best results and was then applied to the blast wave-truck interaction problems in two dimensions. MacCormack's method was also used in three dimensions to determine the flowfield that results when a blast wave strikes a rectangular parallelepiped at an arbitrary angle. Both the twoand three-dimensional computations were compared with experiments in a number of ways. Two dimensional density contours show qualitative agreement for shock front location and Mach stem formation with spark shadowgraphs taken in a shock tube. Pressure-time histories indicate good quantitative agreement between theory and experiment both in two- and three-dimensions.
Document ID
19830044978
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Mark, A.
(U.S. Army, Ballistics Research Laboratories, Aberdeen Proving Ground MD, United States)
Kutler, P.
(NASA Ames Research Center Applied Computational Aerodynamics Branch, Moffett Field, CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1982
Subject Category
Fluid Mechanics And Heat Transfer
Meeting Information
Meeting: Shock tubes and waves; Thirteenth International Symposium
Location: Niagara Falls, NY
Start Date: July 6, 1981
End Date: July 9, 1981
Accession Number
83A26196
Distribution Limits
Public
Copyright
Other

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