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    A method for designing blended wing-body configurations for low wave drag (1992)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A procedure for tailoring a blended wing-body configuration to reduce its computed wave drag is described. The method utilizes an iterative algorithm within the framework of first-order linear theory. Four computed examples are included. In each case, the zero-lift wave drag was reduced without an increase in the drag due to lift.
    Keywords: AERODYNAMICS
    Type: NASA-TP-3261 , L-17095 , NAS 1.60:3261
    Format: application/pdf
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