Brief survey of phenomena and problems which have arisen at National Physical Laboratory, on wings having leading edge sweeps near 50°, and without twist or spanwise change in profile; wing flow at zero, moderate and high lift is discussed in detail; effect of changing flow pattern on overall wing lift, drag, and pitching moment.


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    Title :

    Introduction to flow about plane swept-back wings at transonic speeds


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Rogers, E.W. (author) / Hall, I.M. (author)

    Published in:

    Publication date :

    1960


    Size :

    16 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :