Tests made at Mach 0.60 to 1.20; Reynolds number, based on mean geometric chord, varied from about 2.2×106 to 5.7×106; comparisons are made with data from NASA -- Tech Note D-655 to show effects on longitudinal stability and performance of blunting model nose, leading edge, and ridge line.


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    Title :

    Static longitudinal aerodynamic characteristics at transonic speeds of blunted right triangular pyramidal lifting reentry configuration for angles of attack up to 110°


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    38 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :