About Us ~ What's New
The details of the last six ESDU Data Releases and the current MMDH Supplement are listed below.
Current Status | |
ESDU Data | Release 2023-01 (Jan 2023) |
MMDH | Supplement 49 |
Release 2023-01 (Jan 2023)
- 22002 : Rooke and Cartwright's compendium of stress intensity factorsNew.
- TM 191 : ESDU TECHNICAL MEMORANDUM
Rebound resilience of interface layer - effect of temperature and bearing pressureNew. - TM 196 : ESDU TECHNICAL MEMORANDUM
Asphalt pavement surfaces - Surface temperature and decelerating forcesNew. - TM 201 : ESDU TECHNICAL MEMORANDUM
British Pendulum - use in modelling decelerating-force coefficientsNew. - TM 202 : ESDU TECHNICAL MEMORANDUM
ESDU Tyre modelling - rubber-block forcesNew. - TM 203 : ESDU TECHNICAL MEMORANDUM
British Pendulum - illustration of ESDU modelsNew. - TM 204 : ESDU TECHNICAL MEMORANDUM
Hysteresis and adhesion - an algebraic model deduced from output from a British PendulumNew. - 71026 : Frictional and retarding forces on aircraft tyres. Part II: estimation of braking force.Updated to Amendment E.
- 72008 : Frictional and retarding forces on aircraft tyres.
Part III: planing.Updated to Amendment A. - 90035 : Frictional and retarding forces on aircraft tyres.
Part V: estimation of fluid drag forces.Updated to Amendment B. - TM 174 : ESDU TECHNICAL MEMORANDUM
Correlation of the micro-texture sharpness parameter F1Updated to Amendment B. - TM 211 : ESDU TECHNICAL MEMORANDUM
Pressures under wet footprintUpdated to Amendment A.
Release 2022-04 (Oct 2022)
- 06009 : Fatigue damage and life under random loading.Updated to Amendment B.
- 06010 : Cycle counting methods for the estimation of fatigue life.Re-issue 2.
- 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.
- 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.
- 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
Release 2022-03 (Jul 2022)
- 05001 : Prediction of combustor noise from gas turbine engines.Updated to Amendment C. New/Modified VIEWpac program. New/Modified ESDUpac program.
- 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.
- MMPDS-17 Chapter 1 : Metallic Materials Properties Development and Standardization (MMPDS):
CHAPTER 1 - INTRODUCTIONRe-issue 17.Series: none
Other collections: MMPDS - MMPDS-17 Chapter 2 : Metallic Materials Properties Development and Standardization (MMPDS):
CHAPTER 2 - STEEL ALLOYSRe-issue 17.Series: none
Other collections: MMPDS - MMPDS-17 Chapter 3 : Metallic Materials Properties Development and Standardization (MMPDS):
CHAPTER 3 - ALUMINUM ALLOYSRe-issue 17.Series: none
Other collections: MMPDS - MMPDS-17 Chapter 4 : Metallic Materials Properties Development and Standardization (MMPDS):
CHAPTER 4 - MAGNESIUM ALLOYSRe-issue 17.Series: none
Other collections: MMPDS - MMPDS-17 Chapter 5 : Metallic Materials Properties Development and Standardization (MMPDS):
CHAPTER 5 - TITANIUM ALLOYSRe-issue 17.Series: none
Other collections: MMPDS - MMPDS-17 Chapter 6 : Metallic Materials Properties Development and Standardization (MMPDS):
CHAPTER 6 - HEAT-RESISTANT ALLOYSRe-issue 17.Series: none
Other collections: MMPDS - MMPDS-17 Chapter 7 : Metallic Materials Properties Development and Standardization (MMPDS):
CHAPTER 7 - MISCELLANEOUS ALLOYS AND HYBRID MATERIALSRe-issue 17.Series: none
Other collections: MMPDS - MMPDS-17 Chapter 8 : Metallic Materials Properties Development and Standardization (MMPDS):
CHAPTER 8 - STRUCTURAL JOINTSRe-issue 17.Series: none
Other collections: MMPDS - MMPDS-17 Chapter 9 : Metallic Materials Properties Development and Standardization (MMPDS):
CHAPTER 9 - GUIDELINESRe-issue 17.Series: none
Other collections: MMPDS
Release 2022-02a (May 2022)
- MMPDS-16 Chapter 1 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 1 - INTRODUCTIONNew.Series: none
Other collections: MMPDS - MMPDS-16 Chapter 2 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 2 - STEEL ALLOYSNew.Series: none
Other collections: MMPDS - MMPDS-16 Chapter 3 Vol A (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 3 VOL A - ALUMINUM ALLOYSNew.Series: none
Other collections: MMPDS - MMPDS-16 Chapter 3 Vol B (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 3 VOL B - ALUMINUM ALLOYSNew.Series: none
Other collections: MMPDS - MMPDS-16 Chapter 3 Vol C (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 3 VOL B - ALUMINUM ALLOYSNew.Series: none
Other collections: MMPDS - MMPDS-16 Chapter 4 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 4 - MAGNESIUM ALLOYSNew.Series: none
Other collections: MMPDS - MMPDS-16 Chapter 5 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 5 - TITANIUM ALLOYSNew.Series: none
Other collections: MMPDS - MMPDS-16 Chapter 6 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 6 - HEAT-RESISTANT ALLOYSNew.Series: none
Other collections: MMPDS - MMPDS-16 Chapter 7 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 7 - MISCELLANEOUS ALLOYS AND HYBRID MATERIALSNew.Series: none
Other collections: MMPDS - MMPDS-16 Chapter 8 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 8 - STRUCTURAL JOINTSNew.Series: none
Other collections: MMPDS - MMPDS-16 Chapter 9 (since amended ~ see current version) : Metallic Materials Properties Development and Standardization (MMPDS): CHAPTER 9 - GUIDELINESNew.Series: none
Other collections: MMPDS
Release 2022-02 (May 2022)
- 11003 : Cyclic stress-strain and strain-life properties for metallic materialsNew.
- 22001 : Definitions of terms used in Vibration and Acoustic FatigueNew.
- ASTEROID : Aircraft Surface Tolerances for Enhanced Repair, Operations and DesignNew.Series: Transonic Aerodynamics, Performance, Aerodynamics
Other collections: Aerodynamics Design Collection, Aerospace Package, ASTEROID Collection - 15002 : Definitions for runway contaminants and the classification and distribution of hard runway surfacesUpdated to Amendment A.
- 74036 : Drag due to a circular cavity in a plate with a turbulent boundary layer at subsonic, transonic and supersonic speedsNew/Modified Toolbox App.Series: Aerodynamics
Other collections: Aerodynamics Design Collection, Aerospace Package, ASTEROID Collection - 75028 : Drag due to grooves in a flat plate with a turbulent boundary layer, at subsonic and supersonic speedsNew/Modified Toolbox App.Series: Aerodynamics
Other collections: Aerodynamics Design Collection, Aerospace Package, ASTEROID Collection - 75031 : Drag of two-dimensional steps and ridges immersed in a turbulent boundary layer for Mach numbers up to 3.New/Modified ESDUpac program. New/Modified Toolbox App.Series: Aerodynamics
Other collections: Aerodynamics Design Collection, Aerospace Package, ASTEROID Collection - 99031 : Computer program for estimation of lift curve to maximum lift for wing-fuselage combinations with high-lift devices at low speeds.New/Modified ESDUpac program.Series: Aerodynamics
Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment
Release 2022-01 (Jan 2022)
- 21005 : Summary of Data Items on ControlsNew.Series: Aerodynamics
Other collections: Aerodynamics Design Collection, Aerospace Package, Controls and Flaps Segment - TM 207 : ESDU TECHNICAL MEMORANDUM
Concept and preliminary design
Examples of applying rapid aerodynamic analysis tools to three classic historical configurations designed to similar requirementsNew. - 07001 : Noise transmission into aircraft cabins.Updated to Amendment A. New/Modified ESDUpac program.
- AERO W.S.02.03.02 : Theoretical lift-dependent drag of wings at supersonic speeds.Updated to Amendment C.Series: Aerodynamics
Other collections: Aerodynamics Design Collection, Aerospace Package, Aerofoils and Wings Segment - TM 211 (since amended ~ see current version) : ESDU TECHNICAL MEMORANDUM Pressures under wet footprintNew.
MMDH Supplement 49
- DTD5076, new amendment
- EN2085, new amendment
- EN2116, new specification
- EN2279, new issue
- EN2306, new issue
- EN2387, new issue
- EN2541, new specification
- EN2573, new specification
- EN2681, new issue
- EN2726, new issue
- EN2728, new issue
- EN3120, new specification
- EN3219, new specification
- EN3553, new issue
- EN3678, new specification
- L93, new amendment
- prEN2192, new issue
- prEN2247, new amendment
- prEN2403, new specification
- prEN2418, new issue
- prEN2682, new specification
- prEN3357, new specification
- prEN3471, new specification
- prEN3498, new amendment
- prEN3500, new amendment
- prEN3519, new amendment
- prEN3859, new amendment
- prEN3860, new amendment
- prEN3993, new specification
- prEN4448, new specification
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