ESDU AZ Index: TTIQ
 Effect of Deflection on Control Hinge Moment Derivatives, AERO C.04.01.08
 Analysis of windtunnel data to determine installed tailplane liftcurve slope (Appendix A), 89029
 Average Downwash Angle at Tailplane
 flaps deployed, 97021
 flaps undeployed, 80020
 Calculation of Bending Moment, Loading and Torque on Tailplane in Steady Level Asymmetric Flight
 sideslipping, turning or with failed engine, 01010
 Contribution of Fin and Tailplane Separately to Airframe Noise, 90023
 Deformation of Tailplane in Bending and Twisting Using Assumed Modes, 97032
 Deformation of Tailplane Using Normal Modes, 99033
 Effect of Static Deformation on Tailplane Load Distribution, 96037
 LiftCurve Slope for Installed Tailplane in Subcritical Flow
 estimation for fin or bodymounted, 89029
 LiftCurve Slope for Isolated Tailplane in Subcritical Flow
 effect of twin fins, 91009
 Approximate Estimation for Aeroplanes of Less Than 12 500 lbf Weight to 50 ft
 all forms of propulsion, 82033
 Approximate Estimation of AllEnginesOperating Distance to 35 ft
 multiengined transport aeroplanes, 76011
 Approximate Estimation of Balanced Field Length for Transport Aeroplanes, 76011
 effect of secondsegment climb gradient, 76011
 effect of various levels of deceleration, 76011
 Civil Airworthiness Requirements, 76011, 82033, 85029, 87018
 Detailed Example Calculation Procedure and Results for Typical Transport Aeroplane
 definition of segments and their end points, 87018
 influence of airworthiness requirements on, 87018
 taking account of all factors affecting applied forces and moments, 87018
 Discussion of Decelerating Techniques in Abandoned, 85029
 response times of crew and of mechanical systems, 85029
 thrust decay during turbofan and turbojet rundown, 85029
 use of reverse thrust, 85029
 Estimation in Phases
 airborne distance, PERF EG5/1
 effect of engine failure on distance, PERF EG5/1
 ground run distance, PERF EG5/1
 Estimation of Thrust Variation With Speed
 Fatigue Loading in Ground Run

 see
 Fatigue Loading
 Impingement Drag Due to Tyre Sidespray on Airframe
 Introduction to Data Items on Estimation, 80026
 Prediction of Tyre Sidespray Envelope, 83042
 Reduction of Measured Data, 80009, PERF RG2/1
 Screen
 definition of location for runways with gradient(s), 87018
 VectoredJetThrust Aircraft
 effect of jet pipe temperature limiter on optimisation, 87037
 optimisation of nozzle angle and speed at nozzle rotation, 87037
 optimisation of proportions of ground and airborne segments, 87037
 presentation of ground and airborne distances nondimensionally, 87037
 stepbystep trajectory calculation, 87037
 Lubrication Systems
 Wing Tip

 see
 Wings
 Isotropic
 Laminated

 see
 Delamination
 Airframe Impingement Drag Due to Tyre Sidespray

 see
 Impingement Drag
 Tabulated for Various Petroleum Products, 00016
 Estimation From Pressure Distribution, 82018
 Forced Convection Heat Transfer
 duct flow, AERO 00.03.26
 SelfContained Bearings or Similar Assemblies
 containing concentrated heat sources, 78026, 78027, 78028, 78029, 79002
 Temperature Meet (Cross) Between Streams in Various Types of TwoStream Heat Exchangers, 98005
 Calculation of Runway Temperature from Ambient Pressure and Ambient Temperature, TM 188
 Considerations in Selecting Appropriate Method
 for gas, liquid, solid or surface, 02006
 Methods Available With Typical Designs, Accuracy, Response, Relative Costs and Applicability
 absorption, emission and line reversal spectroscopy, 02006
 bimetallic thermometer, 02006
 capacitance (permittivity) thermometry, 02006
 crayons, labels, paints, and pellets for peak value indication, 02006
 deforming solids for peak value indication, 02006
 density deduced from refractive index measured by light bending, 02006
 eddy current induced heating monitored through resistance change, 02006
 gas themometry by measuring pressure and/or volume, 02006
 infrared radiation, 02006
 Johnson noise power generated by thermal agitation of electron, 02006
 laserinduced fluorescence, 02006
 liquid in glass thermometer, 02006
 magnetic susceptibility and nuclear resonance thermometry, 02006
 quartz crystal vibration, 02006
 remote sensing of radiation with fibreoptic probes, 02006
 resistance including platinum resistance thermometers, 02006
 scattering (CARS, Raman and Rayleigh), 02006
 semiconductor including diode devices, 02006
 speed of sound measurement, 02006
 thermal imaging, 02006
 thermistors, 02006
 thermochromic liquid crystal colour, 02006
 thermocouples, 02006, 06018
 thermographic phosphor fluorescence, 02006
 Effect on Fatigue Limit
 Effect on Fatigue Strength
 see
 Accelerometers
 Acoustic Fatigue
 Adhesives for Bonded Joints
 Aircraft Performance Analysis
 Aircraft Performance Reduction
 Ambient Temperature
 Axes Systems in Aircraft Dynamics and Performance
 Dynamical Similarity
 Failure Criteria
 Flight Testing
 Flowmetering Devices
 Helicopter Performance Analysis
 Materials Properties
 Nondestructive Examination
 Parameter Identification
 Platinum Resistance Thermometers
 Standard Fatigue Loading Sequences
 Statistics
 Temperature Measurement
 Thermistors
 Thermocouples
 Viscometers
 Windtunnel Corrections for Aerofoils
 Windtunnel Corrections for Bluff or Quasistreamlined Bodies
 Windtunnel Corrections for Wings
 Windtunnel Testing
 see
 Runways
 see also
 Refractory Lining Materials
 Definition, 89022
 Internal Flow
 annularsection ducts, 81045
 coils, 78031
 straight pipes, 92003, 93018, AERO 00.02.05
 Use in Bimetallic Thermometer
 Values of Linear Coefficient for Various Materials
 ceramic, metallic and polymer, 84041
 Definition, 70016
 see also
 Temperature Measurement
 Advantages and Limitations, 02006, 06019
 Cost Relative to that of Other Temperature Measuring Techniques, 02006
 Method of Measuring Resistance, 06019
 Resistance/Temperature Relationship, 02006, 06019
 Response Times, 02006, 06019
 SelfHeating Effects (Dissipation Constant), 06019
 Various Types Available and Dimensions, 02006, 06019
 dimensions and temperature range, 06019
 Use in Temperature Measurement
 see also
 Temperature Measurement
 Accuracy According to Class and Type as Result of Manufacturing Tolerances, 02006
 Advantages and Limitations, 02006, 06018
 Calibration, Problems of Checking and Stability, 06018
 Cost Relative to that of Other Temperature Measuring Techniques, 02006
 Discussion of Use of Compensating or Extension Wires, 02006, 06018
 error correction, 06018
 selection of appropriate materials, 06018
 Explanation of Method of Operation, 02006, 06018
 Glossary, 06018
 Heat Treatment of Wires, 06018
 Installation and Checking, 06018
 International Type Designations, 02006, 06018
 Junction Manufacture, 06018
 Material Selection for Sheath, 06018
 Material Selection for Wires, 02006, 06018
 Reference Devices
 advantages and limitations, 06018
 temperature transposition, 02006, 06018
 Response TImes, 02006
 Sensitivity of Various Materials at Various Temperatures, 02006, 06018
 System Design and Check List, 06018
 Typical Output Characteristics, 02006, 06018
 Use With Data Acquisition Systems, 06018
 Definitions, AERO S.00.03.06
 Basic Concepts, AERO S.00.03.06
 Use on Temperature Measurement
 Selection and Use for Dry Rubbing Bearings
 see also
 Aluminium Alloy Bars and Plates
 Aluminium Alloy Sheets
 Austenitic Stainless Steels
 High Alloy Steels
 High Tensile Low Alloy Steels
 Low Tensile Low Alloy Steels
 Martensitic Stainless Steels
 Precipitation Hardening Stainless Steels
 Titanium Alloy (Ti10V2Fe3Al)
 Titanium Alloy (Ti4Al4Mo2Sn0.5Si)
 Titanium Alloy (Ti4Al4Mo4Sn0.5Si)
 Titanium Alloy (Ti6Al4V)
 Pressure Drop Across, 69022
 see also
 Dry Rubbing Bearings
 Ball, Cylindrical or Needle Rolling Element
 FixedInclinedPad Hydrodynamic
 analysis of performance of existing design, 82029, 92034
 choice of pad rise, 82029, 92034
 determination of churning loss, 82029, 92034
 determination of effective film and pad maximum temperatures, 82029, 92034
 determination of film power loss and film thickness, 82029, 92034
 determination of lubricant flow rate, 82029, 92034
 effect of startup requirements on design, 82029, 92034
 initial estimate of dimensions, 82029, 92034
 lubricant feed arrangement, 82029, 92034
 minimum film thickness and effect of misalignment, 82029, 92034
 recommended pad surface finish, 82029, 92034
 Guide to Choice of Type, 67033
 Materials for Hydrodynamic for Industrial Use
 ability to embed particles, 88018
 alloys and forms available, 88018
 causes of contact and effect on life, 88018
 compatibility with counterface material, 88018
 hardness and compatibility with counterface hardness, 88018
 maximum load and operating temperature, 88018
 relative fatigue strength, 88018
 selection procedure to meet operating requirements, 88018
 TiltingPad Hydrodynamic
 analysis of performance of existing design, 83004, 92035
 determination of effective film and pad maximum temperatures, 83004, 92035
 determination of film power loss and churning loss, 83004, 92035
 determination of film thickness, 83004, 92035
 determination of lubricant flow rate, 83004, 92035
 effect of startup requirements on design, 83004, 92035
 initial estimate of dimensions, 83004, 92035
 lubricant feed arrangement, 83004, 92035
 minimum film thickness and effect of misalignment, 83004, 92035
 position of pivot, 83004, 92035
 recommended pad surface finish, 83004, 92035
 see also
 Longitudinal Force
 Windmilling Propellers
 Checklist of Components Affected by Airframe Interference, 85017
 Compatibility of Definition With Drag Definition, 85015, 85017
 Decrement Due to Body Interference With Propeller Flow
 discussion of applicability of prediction method, 86017
 estimation for body with pusher or tractor propeller, 86017
 Definitions
 freeair, net, minimumbody, propulsive, shaft, 85015, 85017
 Discussion of Airframe Interference Effects, 85015, 85017
 induced and profile losses, 85015
 Estimation of Braking, PERF ED1/2
 Estimation of Effect of Small Changes on Level Speed, 86004
 Estimation of Effect of Small Changes on Rate of Climb, 94039
 Estimation of FixedPitch
 effect of forward speed at maximum rotation speed (engine throttled), 83028
 effect of forward speed below speed for maximum rotation speed, 83028
 Estimation of Uninstalled ConstantSpeed, 83001
 effect of activity factor, disc loading, and forward and tip speeds, 83001
 effect of aerofoil section, 83001
 note on estimation of installation effects, 83001
 Approximate Relationship Between Design Specific and ByPass Ratio, 76034
 Compatibility of Definition With Drag Definition, 69006, 81024
 Convergent Nozzle in Altitude Test Facility, TM 189
 Decay After Fuel Supply Cut or Throttle Closure, 85029
 Definitions
 Estimation of Effect of Small Changes on Level Speed, 86004
 Estimation of Effect of Small Changes on Rate of Climb, 94039
 Estimation of Variation With Speed During TakeOff
 effect of ambient conditions, control laws and flat rating, 76034
 effect of intake total pressure loss, 77001
 mixed flow low bypass and turbojet engines with or without reheat, 76034
 unmixed flow engines, 76034
 Interference of Underwing Jet Efflux With MultiSlotted Flap
 estimation of decrement due to, 82034
 Measurement in Flight
 curves for use in, 69008
 gas generator and rake traverse methods, 69007
 introduction to Data Items on, 69006
 static pressure or total head sampling methods, 69007
 Nozzle
 compressible flow equations and curves, 67035, 69008, 81004
 Reverse
 discussion of use to decelerate aircraft, 85029
 Thrustdrag accounting from flight test data
 see also
 Extreme Wind Speeds
 Discussion of Origin and Characteristics, 87034
 see
 Wings
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