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  • 1
    facet.materialart.
    Unknown
    Study of transonic flow over swept wings (1983)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The design of shockless airfoils that are appropriate for experimental work on a supersonic transport with an oblique wing are examined. A series of computer codes for the design and analysis of airfoils and wings in two dimensional and three dimensional transonic flow are studied. The oblique wing 3-D code was the forerunner of the later swept wing code. Techniques to incorporate the effect of an engine or fuselage in the inverse design code while using a minimum of computer resources are developed.
    Keywords: AERODYNAMICS
    Type: NASA-CR-173799 , NAS 1.26:173799
    Format: application/pdf
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