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    Computation of transonic viscous flow past the NTF 65-degree Delta Wing (1993)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: This project is a continuation of the work performed in the summers of 1991 and 1992, during which a 9-block structured grid for the computational domain around each of the four NTF 65-degree Delta Wing models with the sting mount were created. The objective of the project is to validate and supplement the test data on the wing models by computing the viscous flow field about the models.
    Keywords: AERODYNAMICS
    Type: Old Dominion Univ., The 1993 NASA-ODU American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program; p 196-199
    Format: application/pdf
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