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Waverider design for generalized shock geometriesA new design method for waverider configurations with generalized shock geometries is presented. A cross-stream Euler marching procedure is used to define the post-shock flow field, and an arbitrary 3D shock shape is specified as an input. This approach makes it possible to use nonaxisymmetric shock topologies with nonconstant shock strengths. The problem is reformulated in the proper curvilinear coordinate system to suppress its fundamental ill-posedness.
Document ID
19930040861
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jones, K. D. (NASA Langley Research Center Hampton, VA, United States)
Dougherty, F. C. (NASA Langley Research Center Hampton, VA, United States)
Seebass, A. R. (Colorado Univ. Boulder, United States)
Sobieczky, H. (DLR Goettingen, Germany)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 93-0774
Report Number: AIAA PAPER 93-0774
Meeting Information
Meeting: AIAA, Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 11, 1993
End Date: January 14, 1993
Sponsors: AIAA
Accession Number
93A24858
Funding Number(s)
CONTRACT_GRANT: NAG1-1295
Distribution Limits
Public
Copyright
Other

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