Published Toolbox codes

• EPOL v1 update

  'ESDUpacs On Line' codes for simple FIFO Fortran

  • A7011 from Aero, as an example. Replace the 'esduid' parameter for others.

• Aerodynamics

  • 06014: Zero-lift drag coefficient increment due to full-span plain flaps.
    • Toolbox interface to ESDU 06014
  • 08013: Increment in wing profile drag coefficient due to the deployment of a single-slotted flap.
    • Toolbox interface to ESDU 08013
  • 16007: Drag of a rectangular planform cavity, with or without doors, in a flat plate with a turbulent boundary layer for Mach numbers up to 3
    • Toolbox interface to ESDU 16007
  • 70011: Lift-curve slope and aerodynamic centre position of wings in inviscid subsonic flow
    • Toolbox interface to ESDU 70011 - simplified version with single inputs
  • 70012: Lift-curve slope and aerodynamic centre position of wings in inviscid supersonic flow
    • Toolbox interface to ESDU 70012 - simplified version with single inputs
  • 74036: Drag due to circular cavities
    • Toolbox interface to ESDU 74036
  • 75004: Wave drag of wings at zero lift in inviscid airflow
    • Toolbox interface to ESDU 75004
  • 75028: Drag due to grooves in a flat plate with turbulent boundary layer, at subsonic and supersonic speeds
    • Toolbox interface to ESDU 75028
  • 75031: Drag of two-dimensional steps and ridges immersed in a turbulent boundary layer for Mach numbers up to 3
    • Toolbox interface to ESDU 75031
  • 76008: Drag of transverse rows of spherically-headed rivets immersed in a turbulent boundary layer at subsonic and supersonic speeds.
    • Toolbox interface to ESDU 76008
  • 80006: Drag increment due to rear fuselage upsweep
    • Toolbox interface to ESDU 80006
  • 80021: Pressure drag coefficient of blunt forebodies at zero incidence for Mach numbers up to 10.
    • Toolbox interface to ESDU 80021
  • 87005: Increment in aerofoil profile drag coefficient due to the deployment of a single-slotted flap
    • Toolbox interface to ESDU 87005
  • 95009: Effect of wing height on lift and aerodynamic centre for a slender wing-body combination
    • Toolbox interface to ESDU 95009
  • Aero A.02.03.02: Optimum area distribution and associated minimum theoretical transonic drag-rise for aircraft at zero lift
    • Toolbox interface to ESDU Aero A.02.03.02
  • Aero W.05.01.01: Kinetic pressure in the wake behind a wing
    • Toolbox interface to ESDU Aero W.05.01.01
  • Boat-Tail: Subsonic pressure drag of conical boat-tails, incorporating ESDU 77020 and ESDU 76033.
    • Boat-tail
  • International Standard Atmosphere
  • TM169: Wing Lift-Curve Slope
  • Skin Friction Coefficient on a Flat Plate with a Turbulent Boundary Layer

  • ASTEROID

    • ASTEROID - the full version, with various aircraft planforms
    • ASTEROID Flat Plate - a simplified version that deals only with flat plates

  • LiCrA: Lift-Curve Aerodynamics

    • LiCrA 2: High-lift aerofoil codes
    • LiCrA 3: High-lift planform codes

• Strength Analysis:

  • 79016: Inelastic shear stresses and strains in the adhesives bonding lap joints loaded in tension or shear
    • Toolbox interface to ESDU 79016 (with debug options)
  • 89052: Inelastic stress-strain curves app
    • Toolbox interface to ESDU 89052
  • 91008: Strength of lugs under axial load
    • Toolbox interface to ESDU 91008
  • 92041: Stress analysis of single lap bonded joints (adhesive and adherends)
    • Simple Analysis Toolbox interface to ESDU 92041 (with debug options)
    • Flexible Analysis Toolbox interface to ESDU 92041 (with debug options)
  • 93030: Three dimensional stress concentration factors. Plain or countersunk hole in a wide plate subjected to tension, bending or pin loading.
    • Toolbox interface to ESDU 93030
  • 20003: Crack resistance curves app
    • Toolbox interface to ESDU 20003

• Transonic Aerodynamics:

  • VGK: Viscous Garabedian Korn method for two-dimensional aerofoil sections
    • Toolbox interface to ESDU VGK