Flight tests made over lift coefficient range up to about 12.5; characteristics of model without nose jet were satisfactory up to lift coefficient of about 4; of model with nose jet, they were satisfactory over test lift range, but control provided by conventional control surfaces was barely sufficient for maintaining flight at lift of 12.5.


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    Titel :

    Wind-tunnel investigation at low speeds of flight characteristics of sweptback-wing jet-transport airplane model equipped with external-flow jet-augmented slotted flap


    Weitere Titelangaben:

    NACA -- Tech Note


    Beteiligte:


    Erscheinungsdatum :

    1958


    Format / Umfang :

    32 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :