ESDU A-Z Index: SOL-STD

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

Solar Absorptivity

Various Surfaces, 69012, 78029

Solar Heating

Effect on Equilibrium Surface Temperature Due to Aerodynamic Heating, 69009
Effect on Temperatures of Self-Contained Bearing Assemblies, 78029
Total Irradiance Within Atmosphere: scattering and absorption by ozone and water vapour, 69015; scattering by dry atmosphere and dust, 69015; solar constant, 69015; spectral distribution, 69015; variation with altitude, location, season and hour, 69015

Solidity

see: Porosity

Solutions

see: Aqueous Solutions

Sonic Boom

see: Airframe Noise (Aeroplanes Not Propeller Powered)

Sonic Fatigue

see: Acoustic Fatigue

Sonic Flow

Aerofoils: pressure distribution, 69013, TD MEMO 6511
Cones: conditions for existence on surface, 70008, 70009, 70010, AERO S.00.03.16
Wedges: conditions for existence on surface, AERO S.00.03.16

Sonic-Range Pressure Distribution

Aerofoils, 69013, TD MEMO 6511

Sound

see also: Acoustic Absorption Coefficient; Acoustic Impedance; Aircraft Noise Series; Atmospheric Effects on Sound; Crossflow Heat Exchangers; Noise; Noise in Air-Conditioning Duct Systems; Noise Limiting Curves; Noise Prediction for Aerospace Sources; Noise/sound Propagation; Shell-And-Tube Heat Exchangers; Turbo-Fan and Turbo-Jet Engines

Airframe noise, 90023
Boundary layer noise, 75021, TM 58
Buzz-Saw Tones: far-field, 75020; supersonic fan in duct, 75020
Cabin noise, internal noise, 07001
Coaxial Static Subsonic Jet Far-Field: database, 11002; program to interpolate in or extrapolate database, 11002
Combination of Levels, 17012, 79037
Combustor noise, combustion noise, 05001
Conversion to R.M.S. Fluctuating Pressure, 21003
Definitions of Intensity, Intensity Level, Power Level, Pressure and Pressure Level, 21003, 22001
Discrete Frequency Far- and Near-Field for Single Propeller With Axial or Non-Axial Inflow (Static or Flight): estimation of unsteady lift coefficient for input to prediction program, 96027; program for estimation from steady or unsteady loading data, 11005
Discrete Frequency Far-Field for Single Static Propeller/Rotor: graphical estimation of maximum component of rotational noise, 76020
Estimation of Attenuation Due to Barriers: program in Fortran, 79011
Estimation of sideline noise in subjective noise metrics, 82027 Addendum
Fan noise, compressor noise, 98008
Fans: prediction at maximum efficiency point, 79037
Far-field jet noise, 11002, 89041, 98019
Ground reflection effects, 94035
Jet-by-jet noise shielding, 88023
Lateral attenuation, 81035, 82027
Near-field jet noise, 99006
Noise shielding by barriers, 79011
Prediction of Airframe Noise Component-by-Component: program for aeroplanes not propeller powered, 90023
Propeller noise, 11005, 76020, 96027
Section properties of fuselage stiffeners, 07001 Addendum
Shielding Effect of Two Identical Single-Stream Parallel Jets: program for estimation, 88023
Single-Stream Static Jet Far-Field, 89041, 98019: database, 98019; program to interpolate in or extrapolate database, 98019; use of data to predict under flight conditions, 87011
Single-Stream Static Jet Near-Field, 72002, 99006: databases, 99006; program for interpolation in or extrapolation of database, 99006
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 Intensity, 21003
Sound Power, 21003
Sound Pressure, 21003
Sound propagation, 94036
Sound propagation in the presence of wind and temperature gradients, 89036
Sound radiation from circular ducts, 01015
Static-to-flight effects, 87011
Turbine noise, 12001
Turbulent Boundary Layer: surface pressure fluctuations, 75021, TM 58

Spanwise Loading

Due to Change of Angle of Attack, TD MEMO 6403
Effect of Camber and Twist Distributions and Deflection of Leading- and/or Trailing-Edge Plain Flaps on: program for subsonic flow, 95010
Effect of Camber and Twist Distributions on, 83040: program for subsonic flow, 95010
Example of Alleviation by Active Controls, 84020

Spats

Undercarriage

see: Undercarriage Drag Estimation

Specially Orthotropic

Definition, 82013, 83035, 94003

Specific Air Range

see also: Range

Analysis of Flight Test Data to Determine Guarantees: as illustration of use of statistical techniques, 91018
Introduction to Estimation, 73018, 80026
Piston-Engine Aircraft: flight conditions for maximum with parabolic drag law, 75018; practical flight conditions for maximum, 75018; typical variation with operational parameters, 75018
Program to Calculate for Any Power Plant: using known drag and engine characteristics, 00031, 00032, 00033, 00034, 00035, 00036, 00037, 00038, 00039
Turbo-Fan and Turbo-Jet Aircraft: flight conditions for maximum, 73019; flight conditions for maximum with parabolic drag law, 73019
Turbo-Prop Aircraft: flight conditions for maximum with parabolic drag law, 75018; practical flight conditions for maximum, 75018; typical variation with operational parameters, 75018

Specific Endurance

see also: Endurance (Flight Time)

Introduction to Estimation, 73018, 80026
Piston-Engine Aircraft: flight conditions for maximum with parabolic drag law, 75018
Program to Calculate for Any Power Plant: using known drag and engine characteristics, 00031, 00032, 00033, 00034, 00035, 00036, 00037, 00038, 00039
Turbo-Fan and Turbo-Jet Aircraft: flight conditions for maximum, 73019; flight conditions for maximum with parabolic drag law, 73019
Turbo-Prop Aircraft: flight conditions for maximum with parabolic drag law, 75018

Specific Enthalpy of Vaporisation

See under substance of interest

Specific Excess Power

Definition in Aircraft Performance

definition, 70023, 78038, 80026, 80032

Measurement in Flight

see: Anemometric Data Correction

Program to Calculate for Aircraft Performance

using known drag and thrust characteristics, 00031, 00032, 00033, 00034, 00035, 00036, 00037, 00038, 00039

Specific Fuel Consumption

see: Aircraft Piston Engines; Range; Turbo-Fan and Turbo-Jet Engines; Turbo-Prop Engines

Specific Gravity

see: Density

Specific Heat Capacity

see also: Aluminium Alloys; Copper Alloys; Magnesium Alloys; Nickel Steels; Steels; Titanium Alloys

Typical Values for Synthetic Lubricants, 94020
Values for Various Ceramic, Metallic and Polymer Materials, 84041

Specific Heat Capacity Ratio

See under substance of interest

Specific Latent Heat of Vaporisation

See under substance of interest

Specific Range

see: Specific Air Range

Specific Wear Rate

Various Dry Rubbing Bearing Materials: carbon, polymer, thermoset, solid lubricant impregnated metal, 87007

Spectral Analysis

General Introduction to Use in Study of Random Processes

see: Random Processes

Use in Calculating Response of Buildings and Structures

see: Response of Buildings and Structures To Atmospheric Turbulence; Response of Buildings and Structures To Vortex Shedding

Use in Representing Atmospheric Turbulence Properties

see: Turbulence; Turbulence Near Ground

Spectrum Level

see also: Power Spectral Density Function

Definition, 17011
Relation to Power Spectral Density Function, 17011

Speed

see also: Airspeed; Calibrated Airspeed; Equivalent Airspeed; Indicated Airspeed; Indicated True Airspeed; True Airspeed

Analysis of Measurements Made in Level Flight

piston-engine aircraft, 80009

turbine helicopters, 74042, 80009

turbo-fan and turbo-jet aircraft, 70020, 70021, 70022, 80009

Estimation in Level Flight

see also: Equations of Motion

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

program using known drag, lift and thrust characteristics, 00031, 00032, 00033, 00034, 00035, 00036, 00037, 00038, 00039

Estimation of Maximum in Level Flight

program using known drag, lift and thrust characteristics, 00031, 00032, 00033, 00034, 00035, 00036, 00037, 00038, 00039

Measurement in Flight

see: Anemometric Data Correction

Minimum Drag in Level Flight, 81026

Minimum Thrust Power in Level Flight, 81026

Reduction of Measurements Made in Level Flight

piston-engine aircraft, 80009, PERF RP1/0, PERF RP1/1, PERF RP2/0

turbo-fan and turbo-jet aircraft, 80009, PERF RJ2/0

turbo-prop aircraft, 80009, PERF RT1/0, PERF RT1/1

Sound

use in temperature measurement, 02006

Stability During Approach, PERF EG6/2

Spheres

Heat Transfer

see: Free Convection Heat Transfer; Radiation Heat Transfer

Spherical Forebody

see: Forebody

Spherical Roller Bearings

see: Contact Phenomena; Grease in Rolling Bearings; Rolling Bearings

Spherical Shells of Laminated Construction

Under Differential Temperature Across Thickness: steady state temperature and stress distributions, 89027

Spillage Drag

see also: Sidespillage

Axi-Symmetric Cowls at Subsonic Speeds: prediction of onset for all types (NACA 1-series, conical, elliptical, parabolic, other), 84004; prediction of onset (NACA 1-series and with larger lip radius), 81024; variation with geometry and Mach number (NACA 1-series and with larger lip radius), 81024; variation with geometry, Mach number and incidence for all cowls, 84004; variation with Mach number and mass flow ratio (NACA 1-series and modified profiles), 94014
Definition, 81004, 84004, 97016
Flush Intakes: NACA convergent-divergent planform, 86002; rectangular planform, 03006, 86002
Scoop Intakes Immersed in Boundary Layer: with or without boundary layer diverter, 86002

Spiral Coils

see: Forced Convection Heat Transfer; Pressure Drop in Internal Flow

Spiral Mode

Aircraft Lateral Stability and Response

see also: Rolling

discussion of origin and characteristics, 86021

Splined Steel Shaft Assemblies

Fatigue Strength Under Reversed Torsion, 73002: effect of case hardening, form rolling or shot peening, 73002; effect of machining, 73002; effect of number of splines, spline form and spline height, 73002; effect of root radius, 73002
Stress Concentration for Splined Shafts Under Torsion, 73002

Split Flaps

see also: Downwash; Flaps; Interference

Introduction to Data Items on Effect of High-Lift Devices on Drag, Lift and Pitching Moment, 97002
Lift Increment Due to Deployment on Aerofoils at Zero Angle of Attack: alone or with leading-edge high-lift devices, 94026, 94027, 94029
Lift Increment Due to Deployment on Wings at Zero Angle of Attack: alone or with leading-edge high-lift devices, 96032, 97002, 97009
Maximum Lift Increment Due to Deployment on Aerofoils: alone or with leading-edge high-lift devices, 94026, 94027, 94029
Maximum Lift Increment Due to Deployment on Wings, 91014: with leading-edge high-lift devices, 92031
Normal Force, AERO F.05.01.01
Pitching Moment Increment Due to Deployment on Aerofoils and Wings: alone or with leading-edge high-lift devices, 01013, 03017, 98009; flap chord ratio less than unity, AERO F.08.01.01, AERO F.08.01.02
Profile Drag Increment Due to Deployment on Wings, 74010, AERO F.02.01.07
Trailing Vortex Drag Increment Due to Deployment on Cambered and Twisted or Plane Wings: program for estimation for any flap and wing geometry, 01007; tabulated values for selected flap and wing geometries, 01007

Split Roller Bearings

see: Rolling Bearings for Specialised Applications

Splitters

In Bends: design information, 83037; optimum location for one or two in circular-arc, 83037; pressure drop in circular-arc with optimum splitter location, 83037
Use to Improve Diffuser Performance: recommendations for geometry, 87015; static pressure recovery improvement achieved, 87015

Spoilers

Derivation of Part-Span Factors, TM 172
Discussion of Effect of Spoiler Position on Lift-Curve Slope, 14004
Drag Increment in Ground Effect Due to Solid: flaps and slats deployed, 76026
Example of Calculation of Local Excrescence Contribution to Drag, 93032
Induced and Profile Drag Increments in Free Air Due to Perforated or Solid: including contribution to induced drag from flap-spoiler interference, 96026
Lift Decrement in Free Air Due to Perforated or Solid: trailing-edge flaps deployed, 14005; trailing-edge flaps undeployed, 14004
Lift Decrement in Ground Effect: flaps and slats deployed, 76026
Rolling Moment Due to Solid or Perforated: trailing-edge flaps deployed, 14005; trailing-edge flaps undeployed, 14004
Typical Time Delay in Response, 85029
Use with cavity flow, 08011, 08012, 09001, 09002, 16004
Yawing Moment Due to Perforated or Solid Used as Roll Control: including contributions from spoiler-wake-fin and flap-spoiler interferences, 96026

Spray

Prediction of Drag Due to Impingement on Airframe in Take-Off and Landing

see: Impingement Drag

Prediction of Sidespray Envelope From Aircraft Tyres

see: Aircraft Tyres

Springs

see: Disc Springs; Helical Springs of Round Wire; Linkages

Spur Gears

see: Gears

Square Holes with Rounded Corners in Flat Plates

see also: Reinforced Square Holes with Rounded Corners in Flat Plates

Various In-Plane Loadings: stress concentration data, 80027

Square Plates

see also: Boundary Walls and Fences; Flat Plates; Hoardings (Elevated Above Ground Level)

Inclined to Flow

centre of pressure, 70015

normal force, 70015

Normal to Flow

interference effects between pair, 70015

normal force, 70015

shear-flow and surface-mounting effects on forces, 70015

Stress Analysis

see: Curved Square Plates; Flat Specially-Orthotropic Square Plates; Flat Square Plates; Flat Square Plates with Central Circular Hole; Flat Square Plates with Central Flanged Circular Hole

Stress Response to Acoustic Loading

see: Flat Specially-Orthotropic Square Plates

Vibration

see: Flat Specially-Orthotropic Square Plates; Flat Square Plates; Noise

Square-Section Cylinders

Dynamic Response to Turbulence and Wind

see: Response of Buildings and Structures; Response of Buildings and Structures To Atmospheric Turbulence; Response of Buildings and Structures To Vortex Shedding

Mean Forces, Moments and Pressures Due to Wind or Other Fluid Flows

see: Axial Force; Base Pressure; Bluff Bodies; Derivatives; Internal Pressure; Overturning Moment on Surface-Mounted Structures; Pressure Distribution; Profile Drag; Sideforce; Torsional Moment on Structures

Square-Section Diffusers

see: Plane-Walled Diffusers with Single-Plane Expansion

Stability

Boundaries

see: Dynamic Stability; Rolling

Derivatives

see: Derivatives

During Approach, PERF EG6/2

Dynamic

see: Dynamic Stability

In Intake Flow

see: Intakes

In Journal Bearings

see: Journal Bearings

Lateral

see: Lateral Stability and Response

Longitudinal

see: Longitudinal Stability and Response; Pitch-Break (Pitch-Up or Pitch-Down)

Rotors

see: Rotors

Static

see: Longitudinal Stability and Response; Static Aeroelasticity

Structural

see: Buckling

Stacks

Dynamic Response to Turbulence and Wind

see: Response of Buildings and Structures; Response of Buildings and Structures To Atmospheric Turbulence; Response of Buildings and Structures To Vortex Shedding

Mean Forces, Moments and Pressures Due to Wind

see: Base Pressure; Bluff Bodies; Internal Pressure; Normal Force; Overturning Moment on Surface-Mounted Structures; Pressure Distribution; Profile Drag; Sideforce; Torsional Moment on Structures; Vortex Shedding

Mechanical Vibration Characteristics

see: Buildings

Stage Fuel, Length and Time

see: Range

Stagnation Conditions

Curves of as Function of Mach Number: calorically imperfect diatomic gases, AERO S.00.01.10; perfect air, 69026, 73017, 74028, 82018, AERO 00.03.05; perfect gases, 74028, AERO S.00.03.06, AERO S.00.03.07; real air, 73017
Equations for Estimation From Freestream Conditions: pressure only, 73017, 82018; various quantities, 69026, 74028, AERO 00.03.05, AERO S.00.03.06, AERO S.00.03.07

Stainless Steels

see: Austenitic Stainless Steels; Duplex Stainless Steels; High Alloy Steels; Maraging Steels; Martensitic Stainless Steels; Precipitation Hardening Stainless Steels; Steels

Stalling

see also: Flow Separation; Maximum Lift

Considerations in Use of Stall Strips on Wings, 97017
Limitation on Approach Speed, PERF EG6/2
Limitation on Take-Off Safety Speed, 85029

Standard Atmosphere

see: Atmosphere; Equivalent Airspeed; Geopotential Altitude

Standard Deviation

Determination to Specified Confidence for Population From Sample Value: using Chi-Squared Distribution, 91041

Standard Fatigue Loading Sequences

ENSTAFF for Fighter Aircraft Including Environmental Factors: moisture management, 97018; temperature profiles used, 97018
FALSTAFF for Fighter Aircraft: characteristics and mission types, 97018; description of derivation, 97018; general principles in generation of loading, 97018; taxiing loading used, 97018
Felix and Helix for Helicopters: discussion of sortie types, durations and manoeuvres, 97018; landing and take-off loads, 97018; load matrix used, 97018; rainflow analysis, 97018
TWIST and miniTWIST for Transport Aircraft: characteristics, 97018; description of derivation, 97018; flight types and number of cycles used, 97018

Standard Gross/net Thrust

Turbo-Jet Engines

see also: Thrust of Turbo-Fan and Turbo-Jet Engines

definition, 69006

Standard Mean Chord

see also: Aerodynamic Mean Chord; Geometric Mean Chord

Length and Position: straight-tapered wing planforms, or wing planforms with cranks or sawteeth, 10023, 76003, TM 168

Standard Momentum Drag

Turbo-Jet Engines: definition, 69006

Standard Normal Distribution

Definition, 91041

State Variable

Use in Control System Design, 80018

Static Aeroelasticity

Introduction to Influence of Flexibility on Static Stability: constant speed conditions, 96037; overall structural mode, 96037
Treatment of Conventional Transport With Flexible Tailplane/Wing Using Orthogonal Modes: angle of attack in trimmed level flight or a pull-out manoeuvre, 97032; conditions for aeroelastic static stability, 97032; deflections and twist of tailplane and wing, 97032; elevator angle in trimmed level flight or a pull-out manoeuvre, 97032; elevator trim margin in trimmed level flight or a pull-out manoeuvre, 97032; equilibrium equations in quasi-steady symmetric manoeuvres, 97032
Treatment of Flexibility for Conventional Transport With Swept or Unswept Cambered Wing: consideration of elevator trim divergence speed, 96037; effect on tailplane and wing load distribution, 96037; elevator manoeuvre trim margin in steady pull-out, 96037; elevator trim margin in level flight, 96037
Treatment of Flexible Conventional Transport Using Normal Modes: angle of attack in trimmed level flight or a pull-out manoeuvre, 99033; deformation of fuselage, wing, nacelle assembly and tailplane, 99033; elevator angle in trimmed level flight or a pull-up manoeuvre, 99033; equilibrium equations in quasi-steady symmetric manoeuvres, 99033

Static Discharge Wicks

Guidance on Contribution to Excrescence Drag, 94044
Guidance on Number Used on Transport Aircraft, 94044

Static Margin

see: Longitudinal Stability and Response

Static Pressure

see also: Anemometric Data Correction

Calculation of Static Pressure Correction Coefficient, 20006, 20007

In Steady, Spatially Non-Uniform Axial Compressible Flow

as part of reference set of average flow properties for calorically-perfect gas, 95011

as part of reference set of average flow properties for thermally-perfect gas, 97029

Relation With Total Pressure

see: Total Pressure

Variation With Altitude

model atmospheres, 00034, 00036, 68046, 69026, 72018, 77021, 77022, 78008

program to calculate in non-Standard conditions, 00031, 00032, 00033, 00034, 00035, 00036, 00037, 00038, 00039

program to calculate in Standard conditions, 00031, 00032, 00033, 00034, 00035, 00036, 00037, 00038, 00039

Static Pressure Recovery

see: Pressure Recovery

Static Pressure Sensors

see also: Pitot-Static Probes

Measurement of Airspeed, Altitude and Mach Number

see: Anemometric Data Correction

Position (Pressure) Error, 83029, 85036, 86006

sources of, 86006

typical effects on measured airspeed and on measured altitude, 86006

Typical Flow Measurement Errors, 85011

Static Stability

see: Longitudinal Stability and Response

Static Temperature

see also: Ambient Temperature

In Steady, Spatially Non-Uniform Axial Compressible Flow

as part of reference set of average flow properties for calorically-perfect gas, 95011

as part of reference set of average flow properties for thermally-perfect gas, 97029

Relation With Total Temperature in Isentropic Flow

see: Total Temperature

Stationary Process

Definition, 83041

Statistical Energy Analysis

Coupling Loss Factors: equation for connected plates, 15010, 98020, 99009; prediction for curved or flat plates coupled directly or through a beam, 98020
Energy Flow Relationships, 15010
Estimation of Response of Lightweight Structures: advantages, features and limitations, 97033, 99009; commercial software, 15010, 99009; comparison of results for simple structure with those from finite element analysis, 99009; definition and sources of information on modal density, modal overlap and loss factors, 99009; ensemble, frequency and spatial averaging, 99009; experimental determination of parameters from measurements, 99009; introduction to method, 99009; procedure for modelling structure by subsystems and considerations in their definition, 99009; typical applications, 97033, 99009; use of power input, transmission and dissipation to arrive at power balance equations, 99009; variance and its importance in evaluating results, 99009
Modal Density, 11008, 13003, 99009

Statistics

see also: Random Processes; Regression

Anderson-Darling Test for Normality (Goodness of Fit), 91041
Approximate Estimation of Standard Deviation of Output Error From Known System Tolerances, 91017
Chi-Squared Distribution: approximate equations for percentiles, 91041; estimation with specified confidence of population standard deviation from sample value, 91041; table of percentiles, 91017, 91041; use as test for Normality (goodness of fit) 00932 (MMDH), 91017, 91019
Concept of Standard Distributions and Use of Distribution-Free Techniques, 92040
Estimation of Standard Deviation of Variable From Standard Deviation of its Components, 91017, 91020
Explanation of Confidence Level and Probability, FMI2
Extreme-Value Analysis: Gumbel, 87034; Lieblein, 87034; Weibull, 87034
Fisher's Variance Ratio F Distribution: approximate equations for percentiles, 91041; examples of use to establish significance of linear regressions, 92021, 92022; table of percentiles with 95 per cent confidence, 91017; table of percentiles with 97.5 per cent confidence, 91041; use as test for Normality (goodness of fit), 91017, 91018; use for comparison of standard deviations of two samples, 91017, 91018, 91041, 93023
Hypothesis Testing, 91017, 92040
Introduction to Analysis of Engineering Data, 92040
Log-Normal Distribution: cumulative distribution function, 21004; probability density function, 21004
Measures of Dispersion and Location, 92040
Non-Central Student's t Distribution: use in estimation to specified confidence of population coefficient of variation, 91041; use in estimation to specified confidence of population percentiles, 91041
Normal or Gaussian Distribution: approximate equations for percentiles, 91041; Bartlett's test for homogeneity of several estimates of population variance, 91017; bivariate distribution, 91017, 96024; conditional probability distribution, 91017, 96024; cumulative distribution function, 21004; estimation from sample of population coefficient of variation to specified confidence, 91041; estimation to specified confidence of population percentiles from sample mean, 91041; expression for cumulative distribution function, 91041; joint probability distribution, 86010, 91017, 96024; marginal probability distribution, 91017, 96024; probability density function, 21004; probability density function, 85020, 92040; table of statistics for cumulative distribution function and percentiles, 91017, 91041; use of cumulative distribution function to compare means of samples, 93023; use of probability grids, 91017, 91019
Probability Definitions and Relations: random events, and discrete and continuous random variables, 92040
Sampling and Effects of Censoring, 92040
Skewed Distribution, 91017, 92040
Student's t Distribution: equations for percentiles, 91041; estimation to specified confidence of population mean from sample value, 91017, 91041; table of percentiles, 91017, 91041; use for comparison of means of two samples, 91017, 91018, 91041
Techniques of Interval and Point Estimation, and Hypothesis Testing, 92040
Use in Analysis of Atmospheric Turbulence, 74030, 85020, 86010
Use in Analysis of Extreme-Wind Speeds, 87034
Use in Analysis of Two-Phase Flow Pressure Drop Data, FMI2
Use in Deriving Materials Design Data 00932 (MMDH)
Use in Determination of Pressure Error Correction, 95024
Use of Bivariate Distribution in Analysis of Data on Length and Width of US Paved Runways: conditional, joint and marginal distributions, 96024
Use to Analyse Aircraft/Ground-Test Machine Braked Experimental Friction Data: to predict wet stopping distance with chosen probability, 00018, 99015, 99016, 99017
Weibull Distribution: confidence bounds, 21004; cumulative distribution function, 21004; hazard function, 21004; probability density function, 21004; reliability function, 21004; sources of uncertainty, 21004; use in fatigue analysis, 21004; use of probability plots, 21004; Weibull parameters, 21004; Weibull weakest-link theory, 21004

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