Low-speed pressure-recovery and surface-pressure measurements for a twin fuselage-side air-inlet arrangement intended for use at transonic speeds are presented. The model was developed by adding a canopy and nose-wheel fairing to basic transonic annular inlet studied in TN 2685. The results indicate shape requirements of fuselage nose, canopy, and nose-wheel fairing for maintaining substream surface velocities everywhere ahead of entrance.


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    Title :

    A Low-speed Investigation of a Fuselage-side Air Inlet for Use at Transonic Flight Speeds


    Contributors:

    Publication date :

    1952-04-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English