Theory is developed and numerical corrections are computed; at high speeds, corrections are same as those for wing; at low speeds, there is large upwash at rotor; numerical results for two wind-tunnel-wall configurations, one completely closed, and other closed on bottom only.


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    Title :

    Jet-boundary corrections for lifting rotors centered in rectangular wind tunnels


    Additional title:

    NASA -- Tech Report


    Contributors:


    Publication date :

    1960


    Size :

    91 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :