The details of the last six ESDU Data Releases and the current MMDH Supplement are listed below.

• MMPDS-2023 Appendices A-E : Metallic Materials Properties Development and Standardization (MMPDS):
  Appendices A-E
  New.
  Series: none
  Other collections: MMPDS
• MMPDS-2023 Chapter 1 : Metallic Materials Properties Development and Standardization (MMPDS):
  CHAPTER 1 - INTRODUCTION
  Re-issue 2023.
  Series: none
  Other collections: MMPDS
• MMPDS-2023 Chapter 2 : Metallic Materials Properties Development and Standardization (MMPDS):
  CHAPTER 2 - STEEL ALLOYS
  Re-issue 2023.
  Series: none
  Other collections: MMPDS
• MMPDS-2023 Chapter 3A : Metallic Materials Properties Development and Standardization (MMPDS):
  CHAPTER 3A - ALUMINUM ALLOYS
  General through 2000 Series
  Re-issue 2023.
  Series: none
  Other collections: MMPDS
• MMPDS-2023 Chapter 3B : Metallic Materials Properties Development and Standardization (MMPDS):
  CHAPTER 3 - ALUMINUM ALLOYS
  3000 through 7000 Series
  Re-issue 2023.
  Series: none
  Other collections: MMPDS
• MMPDS-2023 Chapter 3C : Metallic Materials Properties Development and Standardization (MMPDS):
  CHAPTER 3 - ALUMINUM ALLOYS
  Cast Alloys and Element Properties
  Re-issue 2023.
  Series: none
  Other collections: MMPDS
• MMPDS-2023 Chapter 4 : Metallic Materials Properties Development and Standardization (MMPDS):
  CHAPTER 4 - MAGNESIUM ALLOYS
  Re-issue 2023.
  Series: none
  Other collections: MMPDS
• MMPDS-2023 Chapter 5 : Metallic Materials Properties Development and Standardization (MMPDS):
  CHAPTER 5 - TITANIUM ALLOYS
  Re-issue 2023.
  Series: none
  Other collections: MMPDS
• MMPDS-2023 Chapter 6 : Metallic Materials Properties Development and Standardization (MMPDS):
  CHAPTER 6 - HEAT-RESISTANT ALLOYS
  Re-issue 2023.
  Series: none
  Other collections: MMPDS
• MMPDS-2023 Chapter 7 : Metallic Materials Properties Development and Standardization (MMPDS):
  CHAPTER 7 - MISCELLANEOUS ALLOYS AND HYBRID MATERIALS
  Re-issue 2023.
  Series: none
  Other collections: MMPDS
• MMPDS-2023 Chapter 8 : Metallic Materials Properties Development and Standardization (MMPDS):
  CHAPTER 8 - STRUCTURAL JOINTS
  Re-issue 2023.
  Series: none
  Other collections: MMPDS
• MMPDS-2023 Chapter 9 : Metallic Materials Properties Development and Standardization (MMPDS):
  CHAPTER 9 - GUIDELINES
  Re-issue 2023.
  Series: none
  Other collections: MMPDS

• 70003 : Local buckling of compression panels with unflanged integral stiffeners.
  Updated to Amendment B.
  Series: Structures
  Other collections: Structures Design Collection, Aerospace Package, Aerostructures Package, Automotive Collection
• 71014 : Local buckling of compression panels with flanged stringers.
  Updated to Amendment B.
  Series: Structures
  Other collections: Structures Design Collection, Aerospace Package, Aerostructures Package, Automotive Collection
• AERO W.05.01.01 : Kinetic pressure in the wake behind a wing.
  Updated to Amendment C. New/Modified ESDUpac program. New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Stability of Aircraft Segment

• 16007 : Computer program for the estimation of the 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
  New.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package
• 23001 : Introduction to ESDU tyre-runway modelling
  New.
  Series: Performance
  Other collections: Aerospace Package
• 23002 : Tyre braking on dry or water-covered runways - summary of ESDU tyre-runway modelling
  New.
  Series: Performance
  Other collections: Aerospace Package
• 23003 : Static braking-force coefficients for tyres on wet and dry surfaces
  New.
  Series: Performance
  Other collections: Aerospace Package
• 23004 : Tyre skidding on dry, paved surfaces
  New.
  Series: Performance
  Other collections: Aerospace Package
• 23005 : Tyre slipping on dry, paved surfaces
  New.
  Series: Performance
  Other collections: Aerospace Package
• 23006 : Tyre skidding on wet, paved surfaces
  New.
  Series: Performance
  Other collections: Aerospace Package
• 23007 : Tyre slipping on wet, paved surfaces
  New.
  Series: Performance
  Other collections: Aerospace Package
• 23008 : Decelerating forces on tyres moving through water or slush
  New.
  Series: Performance
  Other collections: Aerospace Package
• 23009 : Aircraft braking on dry runway
  Application of ESDU 23002
  New.
  Series: Performance
  Other collections: Aerospace Package
• 23012 : Guide to available fatigue crack propagation rate data
  New.
  Series: Fatigue - Fracture Mechanics
  Other collections: Aerospace Package, Aerostructures Package
• TM 205 : ESDU TECHNICAL MEMORANDUM
  Rubber blocks at high pressure
  New.
  Series: Performance
  Other collections: Aerospace Package
• TM 212 : ESDU TECHNICAL MEMORANDUM
  Rigidity modulus for interface material in wet conditions
  New.
  Series: Performance
  Other collections: Aerospace Package
• 00006 : Drag of rectangular planform cavity in a flat plate with a turbulent boundary layer for Mach numbers up to 3. Part I: Closed flow
  Updated to Amendment C. New Interactive Graphs. New/Modified ESDUpac program. New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, ASTEROID Collection
• 00007 : Drag of a rectangular planform cavity in a flat plate with a turbulent boundary layer for Mach numbers up to 3. Part II: Open and transitional flows.
  Updated to Amendment C. New Interactive Graphs. New/Modified ESDUpac program. New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, ASTEROID Collection, Trial Collection
• 05011 : Summary of the model for performance of an aircraft tyre rolling or braking on dry or precipitate contaminated runways.
  Updated to Amendment E.
  Series: Performance
  Other collections: Aerospace Package
• 08011 : Aerodynamics and aero-acoustics of rectangular planform cavities. Part IIIA: Alleviation of unsteady flow effects - Introduction
  Updated to Amendment A.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package
• 10002 : Introduction to worked examples of tyres rolling or braking on dry or precipitate contaminated runways.
  Application of ESDU 05011 and ESDU 13007
  Updated to Amendment C.
  Series: Performance
  Other collections: Aerospace Package
• 10003 : Worked example for tyre in linear motion on a contaminated runway surface.
  An application of ESDU 05011.
  Updated to Amendment C.
  Series: Performance
  Other collections: Aerospace Package
• 10004 : Worked example of ground-test machine operating on a dry or contaminated runway surface.
  Application of ESDU 05011.
  Updated to Amendment C.
  Series: Performance
  Other collections: Aerospace Package
• 10015 : Model for performance of a single aircraft tyre rolling or braking on dry and precipitate contaminated runways
  Updated to Amendment C.
  Series: Performance
  Other collections: Aerospace Package
• 10016 : Drag of a rectangular planform cavity in a flat plate with a turbulent boundary layer for Mach numbers up to 3. Part III : Effect of doors
  Updated to Amendment A. New/Modified ESDUpac program. New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package
• 11004 : Decelerating forces on multiple-wheel undercarriages rolling or braking on precipitate contaminated runways
  Updated to Amendment D.
  Series: Performance
  Other collections: Aerospace Package
• 13002 : Worked example for aircraft with multiple-wheel undercarriages braking on water-covered runway.
  Application of ESDU 11004.
  Updated to Amendment B.
  Series: Performance
  Other collections: Aerospace Package
• 68020 : The compressible two-dimensional turbulent boundary layer, both with and without heat transfer, on a smooth flat plate, with application to wedges, cylinders, and cones.
  Updated to Amendment D.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Aerofoils and Wings Segment
• 80006 : Drag increment due to rear fuselage upsweep.
  Updated to Amendment C. New Interactive Graphs. New/Modified ESDUpac program. New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package
• 94035 : The correction of measured noise spectra for the effects of ground reflection.
  Updated to Amendment E. New/Modified VIEWpac program. New/Modified ESDUpac program.
  Series: Aircraft Noise
  Other collections: Aerospace Package, Noise in Nuclear Facilities
• 97002 : Information on the use of Data Items on high-lift devices.
  Updated to Amendment F.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 70011 : Lift-curve slope and aerodynamic centre position of wings in inviscid subsonic flow.
  New/Modified ESDUpac program. New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Aerofoils and Wings Segment

• 22002 : Rooke and Cartwright's compendium of stress intensity factors
  New.
  Series: Fatigue - Fracture Mechanics, Stress and Strength
  Other collections: Aerospace Package, Aerostructures Package, Nuclear Engineering Package, Nuclear Plant Mechanical/Structural Design
• TM 191 : ESDU TECHNICAL MEMORANDUM
  Rebound resilience of interface layer - effect of temperature and bearing pressure
  New.
  Series: Performance
  Other collections: Aerospace Package
• TM 196 : ESDU TECHNICAL MEMORANDUM
  Asphalt pavement surfaces - Surface temperature and decelerating forces
  New.
  Series: Performance
  Other collections: Aerospace Package
• TM 201 : ESDU TECHNICAL MEMORANDUM
  British Pendulum - use in modelling decelerating-force coefficients
  New.
  Series: Performance
  Other collections: Aerospace Package
• TM 202 : ESDU TECHNICAL MEMORANDUM
  ESDU Tyre modelling - rubber-block forces
  New.
  Series: Performance
  Other collections: Aerospace Package
• TM 203 : ESDU TECHNICAL MEMORANDUM
  British Pendulum - illustration of ESDU models
  New.
  Series: Performance
  Other collections: Aerospace Package
• TM 204 : ESDU TECHNICAL MEMORANDUM
  Hysteresis and adhesion - an algebraic model deduced from output from a British Pendulum
  New.
  Series: Performance
  Other collections: Aerospace Package
• 71026 : Frictional and retarding forces on aircraft tyres. Part II: estimation of braking force.
  Updated to Amendment E.
  Series: Performance
  Other collections: Aerospace Package
• 72008 : Frictional and retarding forces on aircraft tyres.
  Part III: planing.
  Updated to Amendment A.
  Series: Performance
  Other collections: Aerospace Package
• 90035 : Frictional and retarding forces on aircraft tyres.
  Part V: estimation of fluid drag forces.
  Updated to Amendment B.
  Series: Performance
  Other collections: Aerospace Package
• TM 174 : ESDU TECHNICAL MEMORANDUM
  Correlation of the micro-texture sharpness parameter F₁
  Updated to Amendment B.
  Series: Performance
  Other collections: Aerospace Package
• TM 211 : ESDU TECHNICAL MEMORANDUM
  Pressures under wet footprint
  Updated to Amendment A.
  Series: Performance
  Other collections: Aerospace Package

• 06009 : Fatigue damage and life under random loading.
  Updated to Amendment B.
  Series: Vibration and Acoustic Fatigue
  Other collections: Aerospace Package, Aerostructures Package, Automotive Collection, Vibration and Acoustic Fatigue in Nuclear Facilities
• 06010 : Cycle counting methods for the estimation of fatigue life.
  Re-issue 2.
  Series: Vibration and Acoustic Fatigue
  Other collections: Aerospace Package, Aerostructures Package, Automotive Collection, Vibration and Acoustic Fatigue in Nuclear Facilities
• 72024 : Aerodynamic characteristics of aerofoils in compressible inviscid airflow at subcritical Mach numbers.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Aerofoils and Wings Segment
• 83040 : Method for the rapid estimation of spanwise loading of wings with camber and twist in subsonic attached flow.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Aerofoils and Wings Segment
• 84026 : Aerofoil maximum lift coefficient for Mach numbers up to 0.4.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Aerofoils and Wings Segment
• 87031 : Wing angle of attack for zero lift at subcritical Mach numbers.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Aerofoils and Wings Segment, Trial Collection
• 89034 : The maximum lift coefficient of plain wings at subsonic speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Aerofoils and Wings Segment
• 89042 : Body effect on wing angle of attack and pitching moment at zero lift at low speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package
• 91014 : Maximum lift of wings with trailing-edge flaps at low speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 92031 : Maximum lift of wings with leading-edge devices and trailing-edge flaps deployed.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 93019 : Wing lift increment at zero angle of attack due to deployment of single-slotted flaps at low speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 93030 : Three-dimensional elastic stress concentration factors. Plain or countersunk hole in a wide plate subjected to tension, bending or pin loading.
  New/Modified ESDUpac program. New/Modified Toolbox App.
  Series: Structures, Stress and Strength, Fatigue - Endurance Data
  Other collections: Structures Design Collection, Aerospace Package, Aerostructures Package, Nuclear Engineering Package, Nuclear Plant Mechanical/Structural Design, Stress Concentrations Segment, Automotive Collection
• 94027 : Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of various leading-edge high-lift devices at low speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 94028 : Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of a plain trailing-edge flap, with or without a leading-edge high-lift device, at low speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 94029 : Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of a trailing-edge split flap, with or without a leading-edge high-lift device, at low speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 94030 : Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of a single-slotted trailing-edge flap, with or without a leading-edge high-lift device, at low speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 94031 : Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of a double-slotted or triple-slotted trailing-edge flap, with or without a leading-edge high-lift device, at low speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 95021 : Wing lift coefficient increment at zero angle of attack due to deployment of double-slotted or triple-slotted flaps at low speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 96003 : Lift curve of wings with high-lift devices deployed at low speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 96032 : Wing lift coefficient increment at zero angle of attack due to deployment of leading-edge devices at low speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 97003 : Fuselage interference effects on flap characteristics.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 97009 : Wing lift coefficient increment at zero angle of attack due to deployment of trailing-edge split flaps at low speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 97011 : Wing lift coefficient increment at zero angle of attack due to deployment of plain trailing-edge flaps at low speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• 97020 : Slope of aerofoil lift curve for subsonic two-dimensional flow.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Aerofoils and Wings Segment
• 98011 : Aerofoil incidence for zero lift in subsonic two- dimensional flow.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Aerofoils and Wings Segment
• 99031 : Computer program for estimation of lift curve to maximum lift for wing-fuselage combinations with high-lift devices at low speeds.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
• AERO W.01.01.05 : Slope of lift curve for two-dimensional flow.
  New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package, Aerofoils and Wings Segment

• 05001 : Prediction of combustor noise from gas turbine engines.
  Updated to Amendment C. New/Modified VIEWpac program. New/Modified ESDUpac program.
  Series: Aircraft Noise
  Other collections: Aerospace Package
• 95009 : Effect of wing height on lift and aerodynamic centre for a slender wing-body combination.
  Updated to Amendment A. New/Modified ESDUpac program. New/Modified Toolbox App.
  Series: Aerodynamics
  Other collections: Aerodynamics Design Collection, Aerospace Package
• MMPDS-17 Chapter 1 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 1 - INTRODUCTION
  New.
  Series: none
  Other collections: MMPDS
• MMPDS-17 Chapter 2 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 2 - STEEL ALLOYS
  New.
  Series: none
  Other collections: MMPDS
• MMPDS-17 Chapter 3 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 3 - ALUMINUM ALLOYS
  New.
  Series: none
  Other collections: MMPDS
• MMPDS-17 Chapter 4 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 4 - MAGNESIUM ALLOYS
  New.
  Series: none
  Other collections: MMPDS
• MMPDS-17 Chapter 5 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 5 - TITANIUM ALLOYS
  New.
  Series: none
  Other collections: MMPDS
• MMPDS-17 Chapter 6 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 6 - HEAT-RESISTANT ALLOYS
  New.
  Series: none
  Other collections: MMPDS
• MMPDS-17 Chapter 7 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 7 - MISCELLANEOUS ALLOYS AND HYBRID MATERIALS
  New.
  Series: none
  Other collections: MMPDS
• MMPDS-17 Chapter 8 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 8 - STRUCTURAL JOINTS
  New.
  Series: none
  Other collections: MMPDS
• MMPDS-17 Chapter 9 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 9 - GUIDELINES
  New.
  Series: none
  Other collections: MMPDS

• B33, new specification
• EN2469, new issue
• EN3311, new issue
• EN3312, new issue
• EN3340, new specification
• EN3355, new issue
• EN3464, new issue
• EN3470, new specification
• EN3486, new specification
• L37, new specification
• prEN2401, new specification
• prEN2407, new specification
• prEN2690, new specification
• prEN3495, new issue
• prEN3497, new amendment
• prEN3557, new specification
• S513, new specification
• TA10, new issue
• TA21, new issue
• TA3, new amendment
• TA52, new issue
• TA58, new issue