ESDU A-Z Index: AF-AL

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

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Afterbody

see also: Base Drag (without Blowing or Jet Efflux); Base Drag with Central Propulsive Jet; Boat-Tailing; Cowls

Incremental afterbody drag, 16003
Incremental afterbody force, 16003
Planform Areas of Various Shapes and Their Centroids, 77028
Pressure at Downstream End of Boat-Tail on Truncated Circular-Arc or Parabolic-Arc: effect of supersonic Mach number and geometry, 00026
Pressure at Downstream End of Boat-Tail on Truncated Conical: effect of supersonic Mach number and geometry, 00017
Pressure Distribution on Circular-Arc, Conical or Parabolic-Arc (Long Afterbodies): effect of supersonic Mach number and geometry, AERO B.S.05.03.01
Pressure Distribution on Circular-Arc, Conical or Parabolic-Arc (Short Afterbodies): effect of supersonic Mach number and geometry, 00028
Pressure Distribution on Circular-Arc or Parabolic-Arc in Supersonic Flow With Central Jet: base pressure less than pressure on end of boat-tail, 00028, AERO B.S.05.03.01
Pressure Distribution on Conical in Supersonic Flow With Central Jet: base pressure less than pressure on end of boat-tail, 00028, AERO B.S.05.03.01
Pressure Distribution on Truncated Circular-Arc, Conical or Parabolic-Arc (Long Afterbodies): effect of supersonic Mach number and geometry, AERO B.S.05.03.01
Pressure Distribution on Truncated Circular-Arc, Conical or Parabolic-Arc (Short Afterbodies): effect of supersonic Mach number and geometry, 00028
Pressure Distribution on Truncated Circular-Arc or Parabolic-Arc in Supersonic Flow With Central Jet: base pressure less than pressure on end of boat-tail, 00028, AERO B.S.05.03.01
Pressure Distribution on Truncated Conical in Supersonic Flow With Central Jet: base pressure less than pressure on end of boat-tail, 00028, AERO B.S.05.03.01
Pressure Drag on Circular-Arc or Parabolic-Arc in Subsonic or Transonic Flow: effect of Mach number and geometry, 96012
Pressure Drag on Conical or Truncated Conical in Subsonic Flow: effect of Mach number and geometry, 77020; effect of rounding after- to mid-body junction, 77020
Pressure Drag on Conical or Truncated Conical in Supersonic Flow: effect of Mach number and geometry, 79022
Pressure Drag on Conical or Truncated Conical in Transonic Flow: effect of Mach number and geometry, 78041
Pressure Drag on Truncated Circular-Arc or Parabolic-Arc in Subsonic Flow With Central Jet: annular base width greater than 0.05 base diameter, 02012; negligible annular base area, 01012
Pressure Drag on Truncated Circular-Arc or Parabolic-Arc in Subsonic or Transonic Flow: effect of Mach number and geometry, 96012
Pressure Drag on Truncated Circular-Arc or Parabolic-Arc in Supersonic Flow With Central Jet: base pressure less than pressure at end of boat-tail, 00026
Pressure Drag on Truncated (Circular-Arc Running into Conical) in Subsonic Flow With Central Jet: negligible annular base area, 01012
Pressure Drag on Truncated Conical in Supersonic Flow With Central Jet: base pressure less or greater than pressure at end of boat-tail, 00017; base pressure less than pressure at end of boat-tail, 00026
Pressure Drag on Truncated (Parabolic-Arc Running into Conical) in Subsonic Flow With Central Jet: negligible annular base area, 01012
Surface Area and Volume, Tail Angle or Radius of Curvature of Various Shapes and Cross-Sections, 77028
Truncated Circular-Arc, Conical or Parabolic-Arc in Supersonic Flow: boat-tail angle as function of dimensions, 00026, 00028
Wave Drag on Circular-Arc, Conical or Parabolic-Arc: effect of Mach number and geometry, AERO B.S.02.03.02; introduction to estimation methods and effect of cross-section shape, AERO B.S.02.03.01
Wave Drag on Truncated Circular-Arc, Conical or Parabolic-Arc: effect of Mach number and geometry, AERO B.S.02.03.02; introduction to estimation methods and effect of cross-section shape, AERO B.S.02.03.01
Wave Drag on Truncated Circular-Arc, Conical or Parabolic-Arc of Elliptical Cross Section, AERO B.S.02.03.01: effect of Mach number and geometry, AERO B.S.02.03.02

Afterbody-Forebody

see also: Cowls

Interference Wave Drag: conical, ducted conical or parabolic-arc forebody with mid-body, AERO B.S.02.03.08; conical or truncated conical or parabolic-arc afterbody with mid-body, AERO B.S.02.03.08
Planform Areas of Various Shapes and Their Centroids, 77028
Surface Area and Volume, Nose or Tail Angle or Radius of Curvature: various shapes and cross-sections, 77028

Ailerons

see also: Controls (Aerodynamic); Controls (Gap Sealed); Controls (with Gap); Flaps; Hinge Moment

Calculation of Deflection Required in Steady Asymmetric Level Flight: estimation of order of magnitude, 01010; sideslipping, turning or with failed engine, 01010
Estimation of Rolling Moment Due to Plain (L sub xi or C sub l delta a), 88013, 88040
Estimation of Yawing Moment Due to Plain (N sub xi or C sub n delta a), 88029, 88040

Air

see also: Air in Dissociation Equilibrium; Atmosphere

Calculation of Runway Surface Temperature From Air Temperature and Ambient Temperature, TM 188
Compressibility Factor: pressure and temperature variation in gaseous state, 88025
Density: altitude variation in model atmospheres, 68046, 72018, 77021, 77022, 78008
Dynamic Viscosity: altitude variation (- 0.5 km to 80 km) in model atmosphere, 77021, 77022; temperature variation (100 K to 3 000 K) in gaseous state, 73017; temperature variation (215 K to 290 K) in gaseous state, 77021, 77022; temperature variation in liquid state, 66024
Forced Convection Heat Transfer in Ducts: variable gas property effects, 81045, 92003, AERO 00.02.05
Gas Constant, AERO 00.01.09
Kinematic Viscosity: altitude variation (- 0.5 km to 80 km) in model atmosphere, 77021; temperature variation in liquid state, 66024
Mean Free Path: altitude variation (80 km to 1 000 km) in model atmosphere, 77021
Mean Particle Speed: altitude variation (80 km to 1 000 km) in model atmosphere, 77021
Molecular Mass, AERO 00.01.08: altitude variation (80 km to 1 000 km) in model atmosphere, 77021
Molecular Vibrational Temperature, AERO 00.01.09
Sources of Data for Thermodynamic and Transport Properties: in liquid and gaseous states, 87009
Specific Enthalpy: pressure and temperature variation in gaseous state, 88025; temperature variation in gaseous state, AERO 00.01.09
Specific Heat Capacity at Constant Pressure: pressure and temperature variation in gaseous state, AERO 00.01.09
Specific Heat Capacity Ratio: pressure and temperature variation in gaseous state, AERO 00.01.09; temperature variation in gaseous state, AERO 00.01.08
Speed of Sound: altitude variation in model atmospheres, 68046, 72018, 77021, 77022; pressure and temperature variation in gaseous state, 73017; temperature variation in gaseous state, 69026
Thermal Conductivity: altitude variation (- 0.5 km to 80 km) in model atmosphere, 77021; temperature variation (200 K to 1 000 K) in gaseous state, 77031; temperature variation (200 K to 1 500 K) in gaseous state, 99005; temperature variation (215 K to 290 K) in gaseous state, 77021

Air Bearings

see: Gas Bearings

Airborne Distance During Landing

see: Landing

Air Brakes

see also: Spoilers

Centre of Pressure and Normal Force, 70015

Air-Conditioning

Effect of Cabin Pressure and Its Rate of Change on Climb and Descent Profiles

see: Cabin Conditions

Guidance on Contribution to Aircraft Drag, 94044

Noise Generation and Transmission in Ducting

see: Noise in Air-Conditioning Duct Systems

Air-Cooled Heat Exchangers

see also: Heat Exchangers

Detailed Cost Data for Various Fluids as Function of Heat Load and Operating Pressure, 92013: effect of bundle length, tube diameter and type, and operating noise, 94043; use in selection of heat exchanger type for given duty, 92013

Aircraft Dynamics

see: Aerodynamic Loading; Ailerons; Attitude Angles; Axes Systems in Aircraft Dynamics and Performance; Control Systems; Direction Angles; Dutch Roll; Dynamic Stability; Equations of Motion; Handling Qualities; Incidence Angles; Lateral Stability and Response; Linear Systems; Longitudinal Stability and Response; Non-Linear Systems; Notation; Parameter Identification; Rolling; Rudder; Sampled-Data Systems; Static Aeroelasticity

Aircraft Fatigue Loads

see: Fatigue Loading

Aircraft Loading

see: Aerodynamic Loading; Fatigue Loading; Impingement Drag

Aircraft Mass/weight

Typical Breakdown for Civil Transport, 94009
Typical Fuel Weight for Civil Transport, 98013
Typical Wing Structure Weight as Fraction of Start-of-Cruise Weight for Civil Transport, 98013

Aircraft Noise

see: Aircraft Noise Series; Noise Prediction for Aerospace Sources; Noise/sound Propagation

Airframe noise, 90023
Bandwidth correction, 17011
Boundary layer noise, 75021, TM 58
Buzz-saw noise, 75020
Cabin noise, internal noise, 02008, 04023, 07001
Combination of noise levels in dB, 17012
Combustor noise, combustion noise, 05001
Contour Plotting of Wing Reflection Effects, TM 198
Estimation of sideline noise in subjective noise metrics, 82027 Addendum
Fan noise, compressor noise, 98008
Far-field jet noise, 11002, 89041, 98019
Ground reflection effects, 94035
Introduction to aircraft noise, 02020
Jet-by-jet noise shielding, 88023
Jet Engine Installation Effects, TM 198
Lateral attenuation, 81035, 82027
Near-field jet noise, 99006
Noise shielding by barriers, 79011
Prediction Methods, 09009
Propeller noise, 11005, 76020, 96027
Rectangular Planform in Flat Plate, 09001, 09002, 16004
Section properties of fuselage stiffeners, 07001 Addendum
Shock noise from supersonic jets, 13001
Sound absorption coefficients of liners, 74003, 74004
Sound attenuation due to air absorption, 78002, 78003
Sound attenuation in circular ducts, 00012
Sound attenuation in rectangular and annular ducts, 00024
Sound propagation, 94036
Sound propagation in the presence of wind and temperature gradients, 04011, 89036
Sound radiation from circular ducts, 01015
Static-to-flight effects on coaxial jet noise, 14014
Static-to-flight effects on single-stream jet noise, 87011
Turbine noise, 12001
Wing-reflection Effects, TM 198

Aircraft Noise Series

Location of Items in ESDU Series, 00010
Record of Amendments to Items in ESDU Series, 00010

Aircraft Performance Analysis

see also: Aircraft Performance Reduction; Axes Systems in Aircraft Dynamics and Performance; Flight Testing; Helicopter Performance Analysis

Accumulation of rainfall on runway surfaces,, 19005

Aircraft on Wet/Dry or Contaminated Runway, 13002

Atmospheric Data for Use in, 68046, 69026, 72018

Correlation of Changes in Drag-Minus-Thrust and Lift in Airborne Manoeuvre

discussion of effect of landing style, 92020

example plots for wide range of aircraft and powerplants, 92020

from speeds at screen and touch-down, 92020

Detailed Example

using accelerometers, air-data system or inertial system, 79018

Equations for Computation of Atmospheric Data for Use in, 77022

Examples of Use of Statistical Techniques Applied to Measurements

to derive a relation between ground run in landing and approach speed, 92021

to derive certification airborne distance from airborne time, speeds and rates of descent, 92022

to derive changes to second segment climb schedule due to small airframe changes, 93023

to estimate from simulation data probability of a short or long autolanding, 91019

to provide customer guarantees of range from flight test data, 91018

Explanations of Various Corrections to Measurements

effects of buoyancy, flexibility and wind, 79018

Introduction to Data Items on, 80009

Introduction to Use of Statistical Techniques, 91017

Piston-Engine Aircraft

methods available for, 80009

rate of climb, 70023

Rate of Climb

effect of small changes in density, drag, weight, thrust (or power), 94039

Speed in Level Flight

effect of small changes in drag, weight, thrust (or power), 86004

Turbo-Fan and Turbo-Jet Aircraft, 70020, 80009

see also: Buoyancy; Gravitational Acceleration

centre of gravity variation effects, 70020

engine operation effects, 70020

fuel consumption, 70021, 70022

range, 70021, 70022, PERF RJ2/0

rate of climb, 70021, 70023, PERF RJ1/2

Reynolds number effects, 70020

speed in level flight, 70021, 70022

thrust inclination to flight path effects, 70020

thrust measurement in flight, 69006, 69007, 69008

Turbo-Prop Aircraft, 80009

rate of climb, 70023

Vectored-Jet-Thrust

take-off performance, including ski-jump, 87037

Aircraft Performance Estimation

see also: Axes Systems in Aircraft Dynamics and Performance; Cabin Conditions; Endurance (Flight Time); Equations of Motion; Flight Path Optimisation; Ground Performance in Take-Off and Landing; Landing; Range; Rate of Climb; Rolling; Specific Air Range; Specific Endurance; Speed; Take-Off; Turning Manoeuvre

Aircraft on Wet/Dry or Contaminated Runway, 13002
Applications of Data Calculated: in airworthiness, design, flight testing and operations, 80026
Conditions for Minimum Drag and Minimum Power, 81026
Estimation of Effect of Small Changes on Level Speed: drag, weight, thrust (or power), 86004
Estimation of Effect of Small Changes on Rate of Climb: density, drag, weight, thrust (or power), 94039
Estimation of Trim Drag Due to Asymmetry: inoperative engine or other sources, 88006
Estimation of Variability of Characteristic Due to Contributions of Component Variabilities, 91020
Introduction to Data Items on, 80026
Program Using Known Airframe Drag Characteristics and Installed Thrust/Fuel Consumption: point behaviour including specific range and ceiling, 00031, 00032, 00033, 00034, 00035, 00036, 00037, 00038, 00039
Representation of Drag by Simple Laws: parabolic with minimum at zero or at finite lift, 81026
Vectored-Jet-Thrust: take-off performance, including ski-jump, 87037

Aircraft Performance Reduction

see also: Aircraft Performance Analysis; Flight Testing; Helicopter Performance Analysis

Introduction to Data Items on, 80009
Piston-Engine Aircraft, 80009, PERF RP1/0: fuel consumption and range, PERF RP1/3, PERF RP2/0; landing and take-off, PERF RG2/1; rate of climb, PERF RP1/2, PERF RP2/0; speed in level flight, PERF RP1/1, PERF RP2/0
Turbo-Fan and Turbo-Jet Aircraft, 80009: fuel consumption and range, PERF RJ2/0; landing and take-off, PERF RG2/1; rate of climb, PERF RJ2/1; speed in level flight, PERF RJ2/0
Turbo-Prop Aircraft, 80009, PERF RT1/0: fuel consumption and range, PERF RT1/3; landing and take-off, PERF RG2/1; rate of climb, PERF RT1/2; speed in level flight, PERF RT1/1
Vectored-Jet-Thrust: non-dimensional parameters appropriate and their derivation, 87037

Aircraft Performance Series

see: Performance Series

Aircraft Piston Engines

Specific Fuel Consumption: factors affecting, 75018; presentation of data by manufacturers, 75018

Aircraft Tyres

see also: Friction Coefficient; Rubber; Slip Ratio

Accumulation of rainfall on runway surfaces, 19005

Aircraft Tyre on Wet/Dry or Contaminated Runway, 10002, 10003, 10004, 13002

Runway contaminants and the classification and distribution of hard runway surfaces, 15002

Calculation of Runway Temperature From Air Temperature and Ambient Pressure to Determine Rebound Resilience, TM 188

Decelerating Forces on Multiple-Wheel Undercarriages

in line-astern and line-abreast arrangements, 11004

rolling or braking on precipitate contaminated runways, 11004

Design Factors and Effect on Tyre/Runway Braking Friction, 16008

inflation pressure and tread materials and patterns, 16008

Drag When Running Through Slush or Water

multiple tyre undercarriage, 11004

single tyre, 05011, 10015, 15007

Drag When Running Through Slush, Water or Snow, 10002, 10003, 10004

multi-wheel undercarriages rolling or braking, 13002

Mumeter Mk 6: a continuous friction measuring device, TM 167

Operating On A Snow-Covered Runway, 15008

Planing of Aircraft Tyre, Partial Planing, Complete Planing, 15003, 15009

Prediction of Sidespray Envelope for Water and Slush

centre plume from inner edges of side-by-side tyre arrangement, 83042

effect of cross wind or head or tail wind, 83042

effect of tyre chine on height, 83042

side plumes from outer edges of side-by-side tyre arrangement, 83042

side plumes from single tyre, 83042

use of spray alleviation deflectors, 83042

width, height and location of inner and outer edges, 83042

Pressure Under Tyre Footprint on Wet Surface, TM 211

Sidespray Impingement Drag on Airframe

see: Impingement Drag

Yawed Rolling (Unbraked)

yawed tyre on wet or dry runway, 10002, 13007, 15007

Air Data System

Calibration of Pressure Air Data Systems, 20006, 20007

Derivation of Aerodynamic Data for Performance Model from Manoeuvring Flight, TM 190

Guidance on Contribution to Excrescence Drag, 94044

Measurement of Airspeed, Altitude and Mach Number

see: Anemometric Data Correction

Measurement of Temperature

see: Ambient Temperature

Airfoils

see: Aerofoil Coordinates; Aerofoils; Aerofoils with Roof-Top Pressure Distribution; Aerofoils with Supercritical Pressure Distribution

Airforce Coefficients

Aerofoil Oscillating in Heave or Pitch or With an Oscillating Control

see also: Pressure Distribution

forces and moments as function of Mach number and frequency, 81034, 82005

introduction to calculation methods in subsonic or supersonic flow, 82020

lift, pitching moment and hinge moment in subsonic flow, 81034

lift, pitching moment and hinge moment in supersonic flow, 82005

use of aerofoil data in wing flutter calculation, 81034

use to calculate flutter, 82020

Bodies of Revolution Oscillating in Bending, Heave or Pitch

lift distribution and pitching moment as function of frequency, 83010

Relationship With Flutter Derivatives, 81034

Relationship With Indicial Functions, 84020

Airframe Noise (Aeroplanes Not Propeller Powered)

see also: Boundary Layer

Introduction to Origins of Sonic Boom, 02020
Prediction at Sideline Observer Component-by-Component: program for one-third octave or overall sound pressure level, 90023
Typical Break Down of Component Contributions in Landing Configuration, 02020

Air in Dissociation Equilibrium

Compressibility Factor: pressure and temperature variation, AERO 00.01.11, AERO 00.01.12
Density: pressure and temperature variation, AERO 00.01.11, AERO 00.01.12
Dynamic Viscosity: pressure and temperature variation, AERO 00.01.07; temperature variation at atmospheric pressures, 73017
Prandtl Number: pressure and temperature variation, AERO 00.01.07
Real Gas Factor: pressure and temperature variation, AERO 00.01.11, AERO 00.01.12
Specific Enthalpy and Specific Entropy: pressure and temperature variation, AERO 00.01.06, AERO 00.01.11, AERO 00.01.12
Specific Heat Capacity Ratio: pressure and temperature variation, AERO 00.01.06
Speed of Sound: pressure and temperature variation, 73017, AERO 00.01.06, AERO 00.01.11, AERO 00.01.12
Thermal Conductivity: pressure and temperature variation, AERO 00.01.07

Air-Lift Pumps

Introduction to Design Features, 88014
Program to Predict Operating Characteristics, 88014: accuracy, 88014; physical model used, 88014

Air Path

Axis System: determination of aircraft acceleration in, 79018; transformation of parameters to other axis systems, 78038, 85030
Velocity: relationship with flight-path velocity, 79018; relationship with wind speed, 79018

Airspeed

see also: Anemometric Data Correction; Calibrated Airspeed; Equivalent Airspeed; Flow Measurement; Indicated Airspeed; Indicated True Airspeed

Airspeed Calibration, 20006, 20007
Calibration Law for Indicator, 86031
Program for Conversion Between Values in Various Definitions, 00031, 00032, 00033, 00034, 00035, 00036, 00037, 00038, 00039

Air Temperature

see: Ambient Temperature

Airworthiness Requirements

see also: Lateral Stability and Response; Longitudinal Stability and Response

Approach Speeds, PERF EG6/2
Definition of Climb Gradient, 70023
Determination of Airborne Distance in Landing From Regression Applied to Measurements: of airborne time, and screen and touchdown speeds and rates of descent, 92022
Effect on Calculation of Accelerate-Stop and Take-Off Performance: example procedure for typical transport aircraft, 87018
Field Length Factors, 76011, 82033, 84040
Load Factor Requirements For Various Aircraft Types, 94009
Speeds for Landing and Take-Off, 85029
Take-Off Field Lengths and Climb Gradients, 76011
Treated as Constraint in Optimising Complete Sortie: example calculation results, 93021
Wet Runway Accountability, 85029

Alleviation Devices

see: Cavities

Allowable Stresses

see also: Cams; Failure Criteria; Helical Springs of Round Wire

Fatigue Loading: aircraft structures, 70018; design to fatigue limit, 75022; general philosophy, SS1
General Philosophy, SS1
Static Loading: beams and struts, SS3; general philosophy, SS1

Alternating Stress

Definition, 70016

Altimeter

Calibration Laws, 86031

Altitude

Convergent Nozzle in Altitude Test Facility, TM 189

Effect of Cabin Pressure and Allowable Pressure Differential on Aircraft Operational

see: Cabin Conditions

Geopotential

see: Geopotential Altitude

Measurement in Flight

see: Anemometric Data Correction

Pressure

definition, 77022, 86031

Variation of Atmospheric Properties

see: Air

Alumina

see: Ceramics

Alumina-Silica Refractory Linings

see: Refractory Lining Materials

Aluminium

see: Aluminium Alloy Bars and Plates; Aluminium Alloy Forgings; Aluminium Alloy Sheets; Aluminium Alloys; Aluminium-Lithium Alloy Bars; Aluminium-Lithium Alloy Plates and Sheets

Aluminium Alloy Bars and Plates

see also: Aluminium Alloys; Aluminium-Lithium Alloy Plates and Sheets; Fretting Fatigue

Fatigue Crack Propagation Rate, 81031, 92030

see also: Crack Propagation

characteristic slopes of plots against stress intensity factor, 81031

effect of alloy composition and heat treatment, 81031, 92030

effect of corrosive environment, 88007

effect of mean stress (or stress ratio), 81031

summary of available data, 23012

Fatigue Crack Propagation Rate (Short Cracks), 92030

effect of alloy composition and heat treatment, 92030

Threshold Stress Intensity Factor Range

effect of mean stress (or stress ratio), 81031

Aluminium Alloy Forgings

see also: Aluminium Alloys

Fatigue Crack Propagation Rate, 81031

see also: Crack Propagation

characteristic slopes of plots against stress intensity factor, 81031

effect of alloy composition and heat treatment, 81031

effect of corrosive environment, 88007

effect of mean stress (or stress ratio), 81031

summary of available data, 23012

Aluminium Alloys

see also: Aluminium Alloy Bars and Plates; Aluminium Alloy Forgings; Aluminium Alloy Sheets; Aluminium-Lithium Alloy Bars; Aluminium-Lithium Alloy Plates and Sheets; Anodising; Bonded Double-Strap Joints in Clad Aluminium Alloys; Bonded Single-Lap Joints in Clad Aluminium Alloys; Composite Structures; Fretting Fatigue; High-Load Transfer Joints in Aluminium Alloys; Low-Load Transfer Joints in Aluminium Alloys; Lugs (Fatigue Strength); Lugs (Static Strength); Materials Properties; Medium-Load Transfer Joints in Aluminium Alloys; Riveted Lap Joints in Aluminium Alloy Sheets; Skin-Rib Joints in Aluminium Alloys; Skin-Rib Joints in Composite Structures; Welded Attachments in Aluminium Alloys; Welded Longitudinal Joints in Aluminium Alloys; Welded Tee Joints in Aluminium Alloys; Welded Transverse Joints in Aluminium Alloys

Bearing, Torsion and Shear Strengths 00932 (MMDH)

Composition of Specific Specifications 00932 (MMDH)

Corrosion Resistance 00932 (MMDH)

Creep Behaviour and Elongation 00932 (MMDH)

Cumulative Fatigue Damage

predictive accuracy of Palmgren-Miner rule, 69024, 95006

Cyclic Stress-Strain Curves, 11003

Density 00932 (MMDH)

Elastic Modulus in Compression 00932 (MMDH), 76016

Elastic Modulus in Tension 00932 (MMDH)

Elastic Modulus of Rigidity 00932 (MMDH)

Electrical Conductivity 00932 (MMDH)

Exfoliation Corrosion Resistance 00932 (MMDH)

Explanation of Composition and Temper Designation System, 91039

Fatigue Strength

effect of surface finish, FAT E.07.02

Fatigue Strength Improvement Obtained by Shot-Peening, 19004

see also: Shot Peening

behaviour in salt water environment, 19004

effect of fretting fatigue, 19004

effect of post-treatment ageing, polishing or stretching, 19004

effect of pre-treatment ageing or heat treatment, 19004

Fatigue Strength Under Acoustic Loading, 72015

effect of cladding, 72015

Fatigue Strength Under Axial Loading of Notched Specimens, FAT E.07.02

effect of compressive mean stress, 74038

effect of tensile mean stress, FAT E.07.03

Fatigue Strength Under Axial or Bending Loading of Notched or Unnotched Specimens

effect of anodising, 87026

Fatigue Strength Under Bending of Unnotched Specimens, FAT E.07.01

effect of tensile mean stress, FAT E.07.03

Fracture Toughness 00932 (MMDH)

variation with temperature, 96013

Generalised Stress-Strain Curves, 76016

program to compute from modulus and two inelastic points, 89052

Poisson's Ratio 00932 (MMDH)

Proof Stresses in Compression 00932 (MMDH), 76016

Proof Stresses in Tension 00932 (MMDH)

Specific Heat Capacity 00932 (MMDH)

Strain-Life Data, 11003

Stress Corrosion Resistance 00932 (MMDH)

Tensile Strength 00932 (MMDH)

Thermal Conductivity 00932 (MMDH)

Thermal Expansion Coefficient 00932 (MMDH)

Typical Values of Density, Shear Modulus and Young's Modulus, 91001

Use as Hydrodynamic Bearing Materials

guide to selection, 88018

Weldability 00932 (MMDH)

Aluminium Alloy Sheets

see also: Aluminium Alloys; Aluminium-Lithium Alloy Plates and Sheets; Fretting Fatigue

Fatigue Crack Propagation Rate, 83007, 92030

see also: Crack Propagation

characteristic slopes of plots against stress intensity factor, 83007

effect of alloy composition and heat treatment, 83007

effect of corrosive environment, 88007

effect of mean stress (or stress ratio), 83007

summary of available data, 23012

Fatigue Crack Propagation Rate (Short Cracks), 92030

Resistance Curves (R-Curves), 20003

see also: Resistance Curves

effect of material specification, 20003, 20003

Threshold Stress Intensity Factor Range, 83007

effect of mean stress (or stress ratio), 83007

Aluminium-Lithium Alloy Bars

Fatigue Crack Propagation Rate: summary of available data, 23012
Fatigue Crack Propagation Rate (Short Cracks), 92030

Aluminium-Lithium Alloy Plates and Sheets

Fatigue Crack Propagation Rate, 91015, 92030

see also: Crack Propagation

effect of alloy composition and heat treatment, 91015, 92030

effect of corrosive and other environments, 91015

effect of mean stress (or stress ratio), 91015, 92030

summary of available data, 23012

Fatigue Crack Propagation Rate (Short Cracks), 92030

effect of alloy composition and heat treatment, 92030

effect of mean stress (or stress ratio), 92030

Threshold Stress Intensity Factor Range, 91015

effect of mean stress (or stress ratio), 91015

Aluminum

see: Aluminium Alloy Bars and Plates; Aluminium Alloy Sheets; Aluminium Alloys; Aluminium-Lithium Alloy Bars; Aluminium-Lithium Alloy Plates and Sheets

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