ESDU A-Z Index: M-MZ
- Definition, 82020, AERO S.00.03.06
- Definition, 82020, AERO S.00.03.06
- Calibration Law, 86031
- Acceleration Experienced in Climb at Constant, 81046
- values in Off-Standard and Standard atmospheres, 81046
- Calculation from GPS Data and Pressure and Temperature Measurements,, 20006, 20007
- Derivation of Indicated True Airspeed, TM 199
- Effect on Aerodynamic and Flow Characteristics
- Equations for Relationship With Calibrated Airspeed, 81046
- Measurement in Flight
-
- see also
- Anemometric Data Correction
- Program to Convert Values to Other Airspeed Definitions
- in Standard or non-Standard atmosphere, 00031, 00032, 00033, 00034, 00035, 00036, 00037, 00038, 00039
- Static Pressure Correction Coefficient as a Function of, 20006
- Variation With Calibrated Airspeed and Pressure Altitude, 69026
- Variation With Equivalent Airspeed and Pressure Altitude, 69026, 78017
- Definition, AERO S.00.03.06
- Bearing Strength 00932 (MMDH)
- Composition of Specific Specifications 00932 (MMDH)
- Corrosion Resistance 00932 (MMDH)
- Creep Behaviour and Elongation 00932 (MMDH)
- Density 00932 (MMDH)
- Elastic Moduli in Compression and Tension 00932 (MMDH)
- Elastic Modulus of Rigidity 00932 (MMDH)
- Electrical Conductivity 00932 (MMDH)
- Exfoliation Corrosion Resistance 00932 (MMDH)
- Fracture Toughness 00932 (MMDH)
- Poisson's Ratio 00932 (MMDH)
- Proof Stresses in Tension 00932 (MMDH)
- Shear Strength 00932 (MMDH)
- Specific Heat Capacity 00932 (MMDH)
- Stress Corrosion Resistance 00932 (MMDH)
- Tensile Strength 00932 (MMDH)
- Thermal Conductivity 00932 (MMDH)
- Thermal Expansion Coefficient 00932 (MMDH)
- Torsion Strength 00932 (MMDH)
- Weldability 00932 (MMDH)
- Linear Systems With Unity Feedback
- determination from Hall, Inverse Nyquist and Nichols plots, 74021
- Linear System
- definition, 73011
- Examples of Use in Calculating Contribution to Drag of Typical Excrescences on Transport Wing, 93032
- Factor Applied to Drag of Isolated on Flat Plate to Obtain Drag on Aerofoil
- estimation by comparison with calculated values for similar pressure distribution, 87004
- program for calculation when pressure distribution alone is known, 91028
- representation in computation by momentum thickness increment, 87004, 98031
- simplified calculation when pressure distribution alone is known, 91028
- use of Nash and Bradshaw equation, 87004, 90029, 91028
- use of VGK to determine, 87004, 98031
- values for family of aerofoils designed for high drag-rise Mach numbers, 91029
- see also
- Steels
- Fatigue Crack Propagation Rate
-
- see also
- Crack Propagation
- characteristic slopes of plots against stress intensity factor, 84003
- effect of alloy composition and heat treatment, 84003
- effect of mean stress (or stress ratio), 84003
- summary of available data, 23012
- Fatigue Strength at High Endurance
- relationship with tensile strength for unnotched specimens, 88008
- Fatigue Strength Under Bending, 71027
- effect of notches, 71027
- relationship with tensile strength, 71027
- Fracture Toughness
- variation with temperature, 83023
- see
- Statistics
- Definition, 83041
- see also
- Steels
- Fatigue Crack Propagation Rate
-
- see also
- Crack Propagation
- characteristic slopes of plots against stress intensity factor, 84003
- effect of alloy composition and heat treatment, 84003
- effect of mean stress (or stress ratio), 84003
- summary of available data, 23012
- Fatigue Strength Under Bending, 71027
- relationship with tensile strength, 71027
- Fracture Toughness
- variation with temperature, 83023
- Threshold Stress Intensity Factor Range, 84003
- effect of mean stress (or stress ratio), 84003
- Compressible Single-Phase Flow Equations and Curves
- see also
- Cowls
- Pressure Drop Across, 66030
- Dynamic Response to Turbulence and Wind
- Mean Forces, Moments and Pressures Due to Wind
- Mechanical Vibration Characteristics
-
- see
- Buildings
- see also
- Aluminium Alloy Sheets
- Aluminium Alloys
- Copper Alloys
- Dry Rubbing Bearings
- Fracture Toughness
- Gears
- Helical Springs of Round Wire
- Journal Bearings
- Magnesium Alloys
- Nickel Steels
- Refractory Lining Materials
- Steel Sheets
- Steels
- Thrust Bearings
- Titanium Alloy (Ti-10V-2Fe-3Al)
- Titanium Alloy (Ti-11Sn-5Zr-2Al-1Mo)
- Titanium Alloy (Ti-2.5Cu)
- Titanium Alloy (Ti-4Al-3Mo-1v)
- Titanium Alloy (Ti-4Al-4Mo-2Sn-0.5Si)
- Titanium Alloy (Ti-4Al-4Mo-4Sn-0.5Si)
- Titanium Alloy (Ti-5Al-2.5Sn)
- Titanium Alloy (Ti-6Al-2Sn-2Zr-2Mo)
- Titanium Alloy (Ti-6Al-2Sn-4Zr-2Mo)
- Titanium Alloy (Ti-6Al-2Sn-4Zr-6Mo)
- Titanium Alloy (Ti-6Al-4V)
- Titanium Alloy (Ti-6Al-5Zr-0.5Mo-0.25Si)
- Titanium Alloy (Ti-6Al-6V-2Sn)
- Titanium Alloy (Ti-8Al-1Mo-1V)
- Titanium Alloys
- Wear Resistant Surface Coatings and Treatments
- Comparison of Various for Ceramic, Metallic and Polymer Materials, 84041
- Density and Melting or Softening Temperature
- various ceramic, metallic and polymer materials, 84041
- Effective Young's Modulus for Various Materials in Contact, 85027, 89045, 94017
- Effect of Composition on Fatigue Crack Growth Rate
-
- see
- Aluminium Alloy Bars and Plates
- Aluminium Alloy Forgings
- Aluminium Alloy Sheets
- Aluminium-Lithium Alloy Plates and Sheets
- Austenitic Stainless Steels
- Duplex Stainless Steels
- High Alloy Steels
- High Tensile Low Alloy Steels
- Low Tensile Low Alloy Steels
- Maraging Steels
- Martensitic Stainless Steels
- Precipitation Hardening Stainless Steels
- Generalised Stress-Strain Curves, 76014, 76016, 89052
- approximate equations for stress at given strain or given stress-to-tangent modulus ratio, 76016
- equations for, 76016, 89052
- method of determination from limited materials data, 76016
- program to compute from modulus and two inelastic points, 89052
- program to compute stress at given strain or given stress-to-tangent modulus ratio
- use to determine plasticity effects for plate buckling, 83044
- variation of Poisson's ratio in inelastic region, 76016
- Introduction to Data in Handbook 00932 (MMDH)
- Layered Materials Used to Increase Structural Damping
- variation of loss factor and modulus with frequency and temperature, 92001
- Limitations on and Variations of Allowable Stress Data
- effects of directionality, material form and other factors 00932 (MMDH)
- Parameter Relationships Used to Derive Data in Handbook
- general values for bearing, shear and tension ratios 00932 (MMDH)
- use of particular relationships 00932 (MMDH)
- Poisson's Ratio
- estimated values for metallic materials in inelastic region, 76016, 89052
- various ceramic, metallic and polymer materials, 78035, 84041, 85027
- various metallic and polymer materials, 94017, 96002
- Secant Modulus
- definition, 76016
- Specific Heat Capacity
- various ceramic, metallic and polymer materials, 84041
- Standardised Test Procedures 00932 (MMDH)
- temperature measurement and calibration 00932 (MMDH)
- Statistical Derivation of Design Values 00932 (MMDH)
- Tangent Modulus
- relationship to secant modulus for generalised stress-strain curve, 76016, 89052
- Temper Designation System Used in Handbook 00932 (MMDH)
- Thermal Conductivity
- various ceramic, metallic and polymer materals, 84041
- Thermal Expansion Coefficient
- various ceramic, metallic and polymer materals, 84041
- Young's Modulus
- various ceramic, metallic and polymer materials, 78035, 84041, 85027
- various metallic and polymer materials, 94017, 96002
- various piping materials, 83046, 87027
- Aerofoils at Mach Numbers From 0.6 to 0.75, AERO W.01.01.07
- Aerofoils in Low-Speed Flow, 84026, 93015
- angle of attack for, with or without high-lift devices deployed, 96003
- effect of leading-edge roughness, 84026, 93015
- increment due to double-slotted flaps, alone or with leading-edge devices, 94027, 94031
- increment due to leading-edge slotted or unslotted high-lift devices, 94027
- increment due to plain flaps, alone or with leading-edge devices, 94027, 94028
- increment due to single-slotted flaps, alone or with leading-edge devices, 94027, 94030
- increment due to split flaps, alone or with leading-edge devices, 94027, 94029
- increment due to triple-slotted flaps, alone or with leading-edge devices, 94027, 94031
- increment due to vented or unvented Kruger flaps, 94027
- Introduction to Data Items on Effect of High-Lift Devices on
- aerofoils, 94026
- wings, 97002
- Viscous Full-potential (VFP) Method for Three Dimensional Wings and Wing-Body Combinations. Part 4: VFP analysis programs for flow breakdown and forces and loads, 21002
- Wings With Leading-Edge Part- or Full-Span High-Lift Devices
- angle of attack for, 96003
- slotted or unslotted, or vented or unvented Kruger, 92031
- Wings With Spanwise Camber and Twist Distribution
- swept or unswept in subcritical flow without high-lift devices, 89034, 93015
- Wings With Trailing-Edge Part- or Full-Span High-Lift Devices
- angle of attack for, 96003
- plain, slotted or split flaps with leading-edge high-lift devices, 92031
- plain, slotted or split flaps without leading-edge high-lift devices, 91014
- Criteria of Yielding and Failure, STRUCT 02.00.00
- Criteria of Yielding and Failure, STRUCT 02.00.00
- Criteria of Yielding for Ductile Materials under Static Loading, 73004
- see
- Speed
- Criteria of Yielding and Failure, STRUCT 02.00.00
- Criteria of Yielding for Ductile Materials under Static Loading, 73004
- Variation With Altitude in Model Atmosphere, 77021
- Definition, 70016
- Effect on Fatigue Crack Propagation Rate
-
- see
- Aluminium Alloy Bars and Plates
- Aluminium Alloy Forgings
- Aluminium Alloy Sheets
- Aluminium-Lithium Alloy Plates and Sheets
- Austenitic Stainless Steels
- Duplex Stainless Steels
- High Alloy Steels
- High Tensile Low Alloy Steels
- Low Tensile Low Alloy Steels
- Maraging Steels
- Martensitic Stainless Steels
- Precipitation Hardening Stainless Steels
- Titanium Alloy (Ti-2.5Cu)
- Titanium Alloy (Ti-4Al-4Mo-2Sn-0.5Si)
- Titanium Alloy (Ti-5Al-2.5Sn)
- Titanium Alloy (Ti-6Al-4V)
- Titanium Alloy (Ti-6Al-6V-2Sn)
- Titanium Alloy (Ti-8Al-1Mo-1V)
- Titanium Sheets
- Effect on Fatigue Limit
- Effect on Fatigue Strength
-
- see also
- Aluminium Alloys
- Low-Load Transfer Joints in Aluminium Alloys
- Lugs (Fatigue Strength)
- Riveted Lap Joints in Aluminium Alloy Sheets
- Screw Threads
- Titanium Alloy (Ti-5Al-2.5Sn)
- Titanium Alloy (Ti-6Al-4V)
- Titanium Alloy (Ti-6Al-6V-2Sn)
- Welded Joints in Steels
- Welded Longitudinal Joints in Aluminium Alloys
- Welded Longitudinal Joints in Steels Under Axial Loading
- Welded Transverse Joints in Aluminium Alloys
- Welded Transverse Joints in Steels Under Axial Loading
- Welded Transverse Joints in Steels Under Bending
- design calculations, 75022
- notched specimens (semi-range/mean stress diagram), FAT A.00.02
- unnotched specimens (semi-range/mean stress diagram), FAT A.00.01
- use of appropriate constant amplitude data in cumulative damage calculations, 95006
- Effect on Fatigue Strength Under Acoustic Loading
- Effect on Fatigue Strength When Component is Subject to Fretting, 90031
- see
- Balancing of Linkages
- Cams
- Cams with Domed or Flat-Faced Followers
- Cams with Swinging Roller Followers
- Cams with Translating Roller Followers
- Contact Phenomena
- Crank-Rocker Mechanisms
- Elastohydrodynamic Lubrication
- Epicyclic Gear Train
- Force Balancing of Linkages
- Gears
- Geneva Mechanisms
- Helical Springs of Round Wire
- Linkages
- Mechanisms Series
- Moment Balancing of Linkages
- Reduction of Torque Fluctuation in Linkage Drive Shafts
- Slider-Crank Mechanisms
- see also
- Fretting Fatigue
- Various Materials
- ceramic, metallic and polymer, 84041
- see also
- Heat Pipes
- Density
- pressure and temperature variation for saturated gas and liquid, 80017
- Dynamic Viscosity
- pressure and temperature variation for saturated gas and liquid, 80017
- Specific Heat Capacity
- pressure and temperature variation for saturated liquid, 80017
- Specific Latent Heat of Vaporisation
- pressure and temperature variation at saturation, 80017
- Surface Tension
- pressure and temperature variation at saturation, 80017
- Thermal Conductivity
- pressure and temperature variation for saturated liquid, 80017
- Vapour Pressure
- pressure and temperature variation at saturation, 80017
- see
- Cow's Milk
- Definition, 22001
- Contact Phenomena
- calculation of individual stress components in concentrated elastic contacts under combined normal and tangential loading, 85007
- stress fields and failure criteria in concentrated elastic contacts under combined normal and tangential loading, 84017
- Criteria of Yielding
- criteria of yielding and failure, STRUCT 02.00.00
- for ductile materials under static loading, 73004
- Dimensions, Deflections and Stresses for Hertzian Contacts under Combined Normal and Tangential Loading
- guide to use of computer program A9434, 94034
- Reynolds-Prandtl Number Regimes for in Horizontal or Vertical Circular-Section Ducts
- laminar or turbulent flow, 92003
- Definition, 22001
- Acoustic Spaces, 13003
- Beams in Bending, 11008
- Bolotin's Method, 11009
- Circular Plates, 11008
- Curved Panels, 11009
- Definition, 78004, 97033
- Equation for Beam in Bending, 99009
- Equation for Plate in Bending, 99009
- Rectangular Enclosure, 13003
- Rectangular Plates, Isotropic, 11008
- Rectangular Plates, Specially Orthotropic, 11008
- Sandwich Panels, 11008, 11009
- Unstiffened Thin-Walled Circular-Cylindrical Shells, 78004
- see also
- Normal Mode Analysis
- Acoustic
- rectangular enclosure, 13003, 15011
- Coupled
- definition, 22001
- For Lateral and Longitudinal Motion of Aircraft, 86021
- desirable characteristics for good handling qualities, 92006
- Fundamental
- definition, 22001
- Linear System
- calculation, 74019
- determination of damping from frequency response measurements, 90006, 93016
- determination of dominant, 80002
- determination of natural frequency from frequency response measurements, 90006, 93016
- sensitivity to changes in system parameters, 80018
- Normal
- definition, 22001
- use in analysising deformation of flexible aircraft, 99033
- Use of Built-In Cantilever Beam Bending and Twisting
- in static aeroelastic stability analysis, 97032
- Use of Orthogonal in Analysing Deformation of Flexible Aircraft, 97032
- Use to Define Trial Functions in Structure Modelling for Dynamic Response, 97033
- Vibration
- Analysis of Strain Gauge Rosette Data, 72014
- Air in Dissociation Equilibrium, AERO 00.01.11, AERO 00.01.12
- Application to Steady, Spatially Non-Uniform Axial Compressible Flow
- calorically-perfect gas, 95011
- thermally-perfect gas, 97029
- Examples in Use of, AERO S.00.03.27
- see also
- Balancing of Linkages
- Linkages
- Advantages and Limitations of Various Methods Singly or in Combination
- counterweights, 89043
- duplicate linkage added with mirror-image symmetry, 89043
- dyad added, 89043
- inertia counterweights, 89043
- Lanchester Balancer, 89043
- moment balancer, 89043
- Use of Constant Speed Rotating Counterweights For Partial Balance of Planar Linkages
- alignment and mass of pair of weights rotating in same direction, 90007
- alignment, mass and location of generalised Lanchester Balancer, 90007
- Moment of Area Rule, AERO A.S.02.03.01
- Aerodynamic
- expressed as expansion in terms of small perturbations, 67003, 86021
- functional dependence, 86021
- Axes Transformation, 67004, 67036, 78038, 82031, 85030, 86041
- Due to Internal Flow, 81004
- On Aircraft and Components
-
- see
- Aerodynamic Loading
- Bending Moment
- Flutter Derivatives
- Ground Performance in Take-Off and Landing
- Hinge Moment
- Pitching Moment
- Pitching Moment Due To Acceleration in Heave (Mw dot or CMα dot)
- Pitching Moment Due To Pitching (Mq or Cmq)
- Pitching-Moment-Curve Slope (MW or Cmα)
- Rolling Moment
- Rolling Moment Due To Rolling (Lp or Clp)
- Rolling Moment Due To Rudder Deflection (Lζ or Cl Δ r)
- Rolling Moment Due To Sideslip (Lv or Cl β)
- Rolling Moment Due To Yawing (Lr or Clr)
- Similarity Laws
- Yawing
- Yawing Moment Due To Aileron Deflection (Nξ or CnΔa)
- Yawing Moment Due To Rolling (Np or Cnp)
- Yawing Moment Due To Rudder Deflection (Nζ or CnΔr)
- Yawing Moment Due To Sideslip (Nv or Cnβ)
- Yawing Moment Due To Yawing (Nr or Cnr)
- On Buildings and Structures Due to Wind or Other Fluid Flows
- Turbo-Jet Engines
- Compressible Flow Equations and Curves
- Computer Program for Estimation of Spanwise Loading of Wings with Camber and Twist in Subsonic Attached Flow. Lifting-surface Theory. (With Appendix A: Effect of Plain Flaps.), 95010
- Graphical Method for Estimating the Spanwise Distribution of Aerodynamic Centre on Wings in Subsonic Flow, TD MEMO 6309
- Introduction to Unsteady Aerodynamics, 82020
- Method for the Rapid Estimation of Theoretical Spanwise Loading due to a Change of Incidence, TD MEMO 6403
- see also
- Lubricants
- Definition, 71003