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Alford et al., 1959 - Google Patents

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing-sweep airplane configuration

Alford et al., 1959

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Document ID
4458229650915750723
Author
Alford W
Luoma A
Handerson W
Publication year

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Wind-tunnel studies have been made to determine the aerodynamic characteristics of a variable-wing-sweep airplane configuration capable of performing multiple missions. The tests covered the Mach number range from 0.25 to 1.30 for the 75 wing-sweep condition but …
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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots

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