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    Strake/delta wing interactions at high angles of attack (1980)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The method of vortex discretization is used to analyze the interaction of the vorticity generated by a strake, with the flow over a delta wing. The validity of the approach is first established by making comparisons with established methods for dealing with delta wings, after which compound delta planforms are discussed. An understanding of the favorable interference effects normally associated with this type of configuration is obtained and results are presented to quantify the expected lift increments resulting from the strake interaction.
    Keywords: AERODYNAMICS
    Type: NASA-CR-166183 , SU-JIAA-TR-30
    Format: application/pdf
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