ESDU A-Z Index: TIR-TQ
- see also
- Titanium Alloys
- Titanium Sheets
- Effect of Fretting on Fatigue Strength, 88027
- see also
- Titanium Alloys
- see also
- Fretting Fatigue
- Lugs (Fatigue Strength)
- Materials Properties
- Screw Threads
- Skin-Rib Joints in Titanium Alloys
- 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)
- Bearing, Torsion and Shear Strength 00932 (MMDH)
- Composition of Specific Specifications 00932 (MMDH)
- Corrosion Resistance 00932 (MMDH)
- Creep Behaviour and Elongation 00932 (MMDH)
- Cyclic Stress-Strain Curves, 11003
- Density 00932 (MMDH)
- Elastic Moduli 00932 (MMDH)
- Electrical Conductivity 00932 (MMDH)
- Exfoliation Corrosion Resistance 00932 (MMDH)
- Fatigue Crack Propagation Rate (Short Cracks), 92023
- summary of available data, 23012
- Fracture Toughness 00932 (MMDH)
- 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)
- Weldability 00932 (MMDH)
- see also
- Titanium Alloys
- Fatigue Crack Propagation Rate for Bar, 82015
- characteristic slopes of plots against stress intensity factor, 82015
- effect of heat treatment and microstructure, 82015
- summary of available data, 23012
- Fatigue Strength Under Axial Loading, 19001
- Fatigue Strength Under Bending for Forging, 19001
- Threshold Stress Intensity Factor Range, 82015
- see also
- Titanium Alloys
- Fatigue Strength Under Axial Loading, 19001
- see also
- Titanium Alloys
- see also
- Titanium Alloys
- Fatigue Strength Under Axial Loading, 19001
- see also
- Titanium Alloys
- Fatigue Strength Under Axial Loading, 19001
- see also
- Titanium Alloys
- Fatigue Strength Under Axial Loading, 19001
- see also
- Titanium Alloys
- see also
- Titanium Alloys
- Fatigue Strength Under Bending for bar, 19001
- see also
- Titanium Alloys
- Fatigue Strength Under Bending for Rod, 19001
- see also
- Titanium Alloys
- Fatigue Strength Under Axial Loading, 19001
- see also
- Titanium Alloys
- Fatigue Strength Under Bending for Rod, 19001
- see also
- Titanium Alloys
- see also
- Titanium Alloys
- see also
- Titanium Alloys
- Effect of Fretting on Fatigue Strength, 88027
- Fatigue Crack Propagation Rate for Bar, 82015
- characteristic slopes of plots against stress intensity factor, 82015
- effect of mean stress (or stress ratio), 82015
- summary of available data, 23012
- Fatigue Strength Under Bending for Bar, 19001
- effect of notches, 19001
- Threshold Stress Intensity Factor Range for Bar, 82015
- see also
- Titanium Alloys
- see also
- Titanium Alloys
- Fatigue Crack Propagation Rate for Bar and Forgings, 82015
- characteristic slopes of plots against stress intensity factor, 82015
- effect of mean stress (or stress ratio), 82015
- summary of available data, 23012
- Fatigue Crack Propagation Rate for Sheet
- characteristic slopes of plots against stress intensity factor, 89051
- effect of mean stress (or stress ratio), 89051
- summary of available data, 23012
- Fatigue Strength Under Axial Loading for Bar or Sheet, 19001
- effect of notches, 19001
- Fatigue Strength Under Axial Loading for Cast Form, 19001
- effect of notches, 19001
- Fatigue Strength Under Bending for Sheet, 19001
- effect of notches, 19001
- see also
- Titanium Alloys
- Fatigue Strength Under Axial Loading for Bar, 19001
- see also
- Titanium Alloys
- see also
- Titanium Alloys
- see also
- Titanium Alloys
- see also
- Resistance Curves
- Titanium Alloys
- Effect of Fretting on Fatigue Strength, 88027
- Fatigue Crack Propagation Rate for Bar and Forgings, 82015, 92023
- characteristic slopes of plots against stress intensity factor, 82015
- effect of heat treatment and microstructure, 82015
- effect of mean stress (or stress ratio), 82015
- summary of available data, 23012
- Fatigue Crack Propagation Rate for Plate, 82015, 90028, 92023
- characteristic slopes of plots against stress intensity factor, 82015, 90028
- effect of corrosive and other environments, 90028
- effect of heat treatment and microstructure, 82015, 90028
- effect of loading frequency, 90028
- effect of mean stress (or stress ratio), 82015
- summary of available data, 23012
- Fatigue Crack Propagation Rate for Sheet, 89051, 90028, 92023
- characteristic slopes of plots against stress intensity factor, 89051, 90028
- effect of corrosive and other environments, 90028
- effect of heat treatment, 89051
- effect of loading frequency, 90028
- effect of mean stress (or stress ratio), 89051
- summary of available data, 23012
- Fatigue Crack Propagation Rate (Short Cracks) for Bar, 92023
- summary of available data, 23012
- Fatigue Crack Propagation Rate (Short Cracks) for Plate, 92023
- summary of available data, 23012
- Fatigue Crack Propagation Rate (Short Cracks) for Sheet, 92023
- summary of available data, 23012
- Fatigue Strength Improvement Obtained by Shot Peening, 19004
-
- see also
- Shot Peening
- behaviour with fretting and at elevated temperature, 19004
- Fatigue Strength Under Acoustic Loading, 10011
- Fatigue Strength Under Axial Loading for Cast Form, 19002
- effect of machining, 19002
- effect of mean stress, 19002
- effect of notches, 19002
- effect of shot peening, 19002
- Fatigue Strength Under Axial Loading for Extruded Form, 19002
- effect of mean stress, 19002
- effect of notches, 19002
- Fatigue Strength Under Axial Loading or Bending for Bar, Rod or Sheet, 19002
- effect of annealing, 19002
- effect of mean stress, 19002
- effect of notches, 19002
- effect of or forging, 19002
- effect of solution treatment and age hardening, 19002
- Resistance Curves (R-Curves), 20003
- Threshold Stress Intensity Factor Range for Bar, Forgings and Plate, 82015
- effect of mean stress (or stress ratio), 82015
- see also
- Titanium Alloys
- see also
- Titanium Alloys
- Fatigue Crack Propagation Rate for Plate, 82015
- characteristic slopes of plots against stress intensity factor, 82015
- effect of heat treatment and microstructure, 82015
- effect of mean stress (or stress ratio), 82015
- summary of available data, 23012
- Fatigue Crack Propagation Rate for Sheet, 90028
- characteristic slopes of plots against stress intensity factor, 90028
- effect of corrosive and other environments, 90028
- effect of loading frequency, 90028
- summary of available data, 23012
- Fatigue Strength Under Axial Loading for Bar or Plate, 19001
- effect of mean stress (or stress ratio), 19001
- effect of notches, 19001
- Fatigue Strength Under Axial Loading for Forgings, 19001
- effect of notches, 19001
- see also
- Titanium Alloys
- Fatigue Crack Propagation Rate for Plate, 82015, 90028
- characteristic slopes of plots against stress intensity factor, 90028
- effect of corrosive and other environments, 90028
- effect of heat treatment, 90028
- effect of loading frequency, 90028
- summary of available data, 23012
- Fatigue Crack Propagation Rate for Sheet
- characteristic slopes of plots against stress intensity factor, 89051
- effect of heat treatment, 89051
- effect of mean stress (or stress ratio), 89051
- effect of thickness, 89051
- summary of available data, 23012
- Threshold Stress Intensity Factor Range for Plate, 82015
- see also
- Titanium Alloys
- Fatigue Strength Under Bending for Bar, 19001
- see also
- Titanium Alloys
- see also
- Titanium Alloys
- see also
- Titanium Alloys
- Fatigue Strength Under Axial Loading for Bar or Plate, 19001
- see also
- Interference Fit
- Bolted Joints
- effect of tilted nut seating on fatigue strength of steel screw threads, 67034
- effect on load distribution with bolt pretension, 13015, 13016, 85021
- Calculation of Effect on a Parameter
- of variabilities of component contributions, 91017
- Effect on Flexural Buckling of Struts, 88034, 90002, STRUCT 01.01.01
- Effect on Locking With Double Lock Nuts, 14002
- Effect on Stress Concentration Due to Double Radius Fillets
- round rods and tubes, 75033
- 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
- variation along saturation curve, 80017
- Discussion of Origin and Characteristics, 87034
- Use to Pretension Bolted Joints
-
- see
- Bolted Joints
- Description of Behaviour of Flat Panels Under Compression, 72012
- Struts Under Compression
- see also
- Aerodynamic Loading
- Beams of Angle Section
- sources of data for two-dimensional crossflow, 82007
- Beams of H-Section
- sources of data for two-dimensional crossflow, 82007
- Lattice Towers of Flat-Sided and/or Tubular Members, 81028
- effect of ancillary components, 81028
- Rectangular-Section Cylinders Normal to Flow
- effect of incidence in turbulent shear flow, 80003
- effect of section aspect ratio in turbulent shear flow, 80003
- Square-Section Cylinders Normal to Flow
- effect of incidence in turbulent shear flow, 80003
- Dynamic Response of Buildings and Structures to Turbulence and Wind
- see also
- Angle Sections with Bulbs
- Definition, STRUCT 00.07.00
- see also
- Anemometric Data Correction
- Behind Normal Shock Wave in Hypersonic Flow
- ratio to static pressure, 93020
- 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
- Isentropic Flow of Calorically Imperfect Diatomic Gas
- effect of characteristic vibrational temperature, AERO S.00.01.10
- variation with Mach number, AERO S.00.01.10
- Isentropic Flow of Perfect Gas
- variation with Mach number and specific heat capacity, 74028, AERO S.00.03.06, AERO S.00.03.07
- variation with Mach number in air, 69026, 73017, 74028, 82018, AERO 00.03.05
- Isentropic Flow of Real Air
- variation with Mach and Reynolds numbers, 73017
- Measurement of During Flight Testing, 20006
- 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
- Isentropic Flow of Calorically Imperfect Diatomic Gas
- effect of characteristic vibrational temperature, AERO S.00.01.10
- variation with Mach number, AERO S.00.01.10
- Isentropic Flow of Perfect Gas
- relation with static temperature, 74028
- variation with Mach number and specific heat capacity, 74028, 97017, AERO S.00.03.06, AERO S.00.03.07
- variation with Mach number in air, 69026, 74028, AERO 00.03.05
- Isentropic Flow of Real Air
- variation with Mach and Reynolds numbers, 73017
- see
- Landing
- Dynamic Response to Turbulence and Wind
- Mean Forces and Moments Due to Wind
- Mechanical VIbration Characteristics
-
- see
- Buildings
- Dynamic Response to Turbulence and Wind
- Mean Forces, Moments and Pressures Due to Wind
- Mechanical Vibration Characteristics
-
- see
- Buildings