Synonyme wurden verwendet für: SPLIT
Suche ohne Synonyme: keywords:(WING FLAPS, SPLIT - PARTIAL-SPAN (20% CHORD))

1–9 von 9 Ergebnissen
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    Wind-Tunnel Investigation of an NACA 23012 Airfoil with a 30 Percent Chord Maxwell Slate and with Trailing-Edge Flaps

    Mckee, John W | NTRS | 1941
    Schlagwörter: WING FLAPS, SLOTTED - FULL-SPAN (25 66%-CHORD) , WING SLATS & FLAPS, SLOTTED & SPLIT , WING FLAPS, SPLIT - FULL-SPAN (20%-CHORD) , WING SLOTS - EFFECT OF GAP , WING SLOTS, MAXWELL & FLAPS, SLOTTEED & SPLIT , WING SLOTS - MAXWELL

    Wind-tunnel investigation of an NACA 23012 airfoil with an 18.05 percent chord Maxwell slat and with trailing-edge flaps

    Mckee, John W | NTRS | 1941
    Schlagwörter: WING FLAPS, SLOTTED - FULL-SPAN (25 66%-CHORD) , WING SLATS & FLAPS, SLOTTED & SPLIT , WING FLAPS, SPLIT - FULL-SPAN (20%-CHORD) , WING SLOTS - EFFECT OF GAP , WING SLOTS, MAXWELL & FLAPS, SLOTTED & SPLIT , WING SLOTS - MAXWELL

    Wind-Tunnel Tests of Two Tapered Wings with Straight Trailing Edges and with Constant-Chord Center Sections of Different Spans

    Neely, Robert H | NTRS | 1943
    Schlagwörter: AIRFOILS - NACA 230 - CHAR & MOMENTS - WING FLAPS, SPLIT , WINGS, TAPERED - CHARACTERISTICS - EFFECT OF WING FLAPS , WING FLAPS, SPLIT-FULL-SPAN VS PARTIAL-SPAN (20%-CHORD) , AIRFOILS - NACA 23015-09 - CHAR & MOMENTS WING FLAPS, SPLIT

    Wind tunnel investigation of effect of yaw on lateral-stability characteristics IV : symmetrically tapered wing with a circular fuselage having a wedge-shaped rear and a vertical tail

    Wallace, Arthur R | NTRS | 1942
    Schlagwörter: MONOPLANES, MID-WING VS HIGH- & LOW-WING , WINGS, TAPERED - CHARACTERISTICS EFFECT OF WING FLAPS , WING FLAPS, SPLIT - PARTIAL-SPAN (20% CHORD)

    Experimental Determination of the Yawing Moment Due to Yawing Contributed by the Wing, Fuselage, and Vertical Tail of a Midwing Airplane Model

    Mathews, Ward O | NTRS | 1943
    Schlagwörter: WING FLAPS, SPLIT - PARTIAL-SPAN (20%-CHORD) , MONOPLANES, MIDWING VS HIGH- & LOW-WING

    Wind-tunnel investigation of effect of yaw on lateral-stability characteristics V : symmetrically tapered wing with a circular fuselage having a horizontal and a vertical tail

    Turner, Thomas R | NTRS | 1943
    Schlagwörter: WINGS, TAPERED - CHARACTERISTICS EFFECT OF WING FLAPS , WING FLAPS, SPLIT - PARTIAL-SPAN (20%-CHORD)

    Tests of a 1/14-Scale Powered Model of the XB-36 Airplane in the Langley 19-Foot Pressure Tunnel I : Stalling Characteristics and Aileron Effectiveness of Several Wing and Flap Arrangements

    Sivells, James C | NTRS | 1945
    Schlagwörter: WING FLAPS, SPLIT - BALANCED , WING SPOILERS , WING FLAPS, SLOTTED - PARTIAL-SPAN , WING FLAPS, FULL-SPAN

    Calculated and Measured Turning Performance of a Navy F2A-3 Airplane as Affected by the Use of Flaps

    Clousing, Lawrence A. / Gadeberg, Burnett L. / Kauffman, William M. | NTRS | 1943
    Schlagwörter: WING FLAPS - DEFLECTION , WING FLAPS, SPLIT - PARTIAL-SPAN

    Effect of Compressibility on Normal-force, Pressure, and Load Characteristics of a Tapered Wing of NACA 66-series Airfoil Sections with Split Flaps

    West, F E / Hallisy, J M | NTRS | 1948
    Schlagwörter: WING FLAPS, SPLIT , WING FLAPS, SPLIT - FULL-SPAN VS PARTIAL-SPAN