An investigation of the air-stream fluctuations at the tail of the D-558-1 airplane has been made at high speed for the purpose of determining the vertical region in which the horizontal tail may be placed without becoming subject to tail buffeting. The investigation was made for a range of Mach numbers from 0.775 to 0.907, and a range of vertical positions at the tall to include two proposed horizontal-tail positions. The tests were made at two angles of attack, 0,2 deg. and 4.2 deg., representative, of the angles of attack for high-speed level flight and a pull-out condition.


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    Titel :

    High-Speed Wind-Tunnel Tests of a 1/16-Scale Model of the D-558 Research Airplane Air-Stream Fluctuations at the Tail of the D-558-1 Airplane


    Beteiligte:

    Erscheinungsdatum :

    1947-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    High-speed wind-tunnel tests of twin-fuselage pursuit airplane

    Anderson, J.L. / Tkac, V.B. | Engineering Index Backfile | 1946



    High-speed wind-tunnel tests of a twin-fuselage pursuit airplane

    Anderson, Joseph L. / Tkac, Victor B. | TIBKAT | 1946