B-24H 42-50363 T8-O “SECTION 8”

B-24H Liberator 42-50363

B-24H 42-50363 damaged in the bomb dump explosion at Metfield 15 July 1944. 491st BG, 853rd BS

The horizontal and vertical tail surfaces of the B-24 Liberator were critical components that contributed to the aircraft’s stability, control, and overall aerodynamic performance. Detailed breakdown of their specifications and features:

Horizontal Tail Surfaces:

  1. Airfoil and Area:

    • Airfoil Section: NACA section No 0015.
    • Total Area: 192 square feet.
    • Span: 26 feet.
    • Maximum Chord: 7 feet 8 3/16 inches.
  2. Position and Stability:

    • Distance from CG: The distance from the design gross weight center of gravity (assumed at 25% MAC) to the one-third maximum chord point was 33.40 feet, approximately 3.5 times the MAC (Mean Aerodynamic Chord).
    • Stabilizer Area: Including elevator balance, the stabilizer area was 140.5 square feet.
    • Setting: The stabilizer’s normal setting relative to the longitudinal axis was 2.5 degrees.
  3. Elevator:

    • Area: 67.1 square feet (51.5 square feet aft of the hinge line).
    • Movement: 30 degrees up and 20 degrees down.
    • Balance: Aerodynamically balanced with all span-wise elements statically balanced about the hinge line.
    • Tabs: Located on the trailing edge, these tabs had an area of 4.95 square feet and were controlled by an irreversible mechanism.

Vertical Tail Surfaces:

  1. Airfoil and Area:

    • Airfoil Section: NACA section 0007.
    • Fin Area: 123 square feet.
    • Rudder Area: 48.8 square feet.
  2. Rudder:

    • Balance: Aerodynamically and statically balanced about the hinge line.
    • Tabs: Total area of 3.1 square feet, equipped with irreversible controls.
    • Movement: 10 degrees right and left of center.

Construction and Features:

  1. Materials and Structure:

    • Control Surfaces: Made of aluminum torque box and rib construction, covered with fabric.
    • Stabilizer: Constructed as a separate assembly with a smooth sheet metal skin, attached to the fuselage with only four fittings for easy replacement.
  2. Positioning:

    • The entire tail assembly was mounted just forward of the tail gunner’s compartment, ensuring the trailing edge did not obstruct the gunner’s vision.

Published at 1272 × 994 px.
Link to full-size photo:
B-24H 42-50363 T8-O “SECTION 8”

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