Zero-Lift Drag of 60° Delta-Wing -- Body Combination (AGARD Model 2) Obtained from Free-Flight Tests Between Mach Numbers of 0.8 and 1.7.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Zero-lift Drag of 60° Delta-wing -- Body combination (AGARD Model 2) obtained from free-flight tests between mach numbers of 0.8 and 1.7


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1954


    Size :

    11 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English