ESDU A-Z Index: J-JZ
- Variation of Buckling Load With Geometry and Stiffness, STRUCT 01.01.24
- see also
- Jet Mixing
- Jet Noise
- Compressible Flow Equations and Curves
- Diffusers
-
- see
- Flow Separation
- Subsonic Heated Jet Parallel to Freestream
- axial and radial velocities, and jet boundaries, AERO A.08.01.09
- Coaxial Static Subsonic Jet Far-Field
- database for circular nozzle mixing, 11002
- effect of distance from and angle to efflux plane, 11002
- effect of primary jet velocity and velocity ratio, 11002
- effect of primary nozzle area and area ratio, 11002
- Introduction to Sources
- jet mixing, shock (or shock-assiciated), and entropy, 02020
- Prediction in Flight Using Data From Single-Stream Circular Static Nozzle
- correction method for jet refraction, amplitude and frequency, 87011
- structure of file used to link ESDU Noise Sub-series programs, 87011
- Shielding Effect of Two Identical Single Stream Parallel Effluxes
- effect of distance from and angle to efflux plane, 88023
- effect of jet area and jet separation, 88023
- effect of jet velocity, density and temperature, 88023
- program predicting shielding level in one-third octave bands, 88023
- Single-Stream Subsonic Static Jet Far-Field
- database for circular nozzle mixing, 98019
- definition of standard error (used to assess accuracy of prediction), 98019
- effect of distance from and angle to efflux plane, 89041, 98019
- effect of jet velocity and temperature, 89041, 98019
- effect of nozzle area, 89041, 98019
- graphical estimation method using model test database, 89041
- method of smoothing used by prediction program in accessing database, 98019
- method of weighting applied by prediction program in using database, 98019
- structure of file used to link ESDU Aircraft Noise Series programs, 98019
- Single-Stream Subsonic Static Jet Near-Field
- database for circular nozzle subsonic mixing, 72002, 99006
- database for circular nozzle supersonic mixing, 99006
- definition of standard error (used to assess accuracy of prediction), 99006
- effect of ambient conditions and nozzle diameter, 99006
- effect of jet velocity and temperature, 99006
- effect of location in noise field, 99006
- estimation based on correlation of model test data, 72002
- graphical estimation method, 72002
- method of smoothing used by prediction program in accessing database, 99006
- method of weighting applied by prediction program in using database, 99006
- program for interpolation in or extrapolation of database, 99006
- structure of file used to link ESDU Aircraft Noise Series programs, 99006
- Typical Spectra of Jet Mixing and Shock-Associated Contributions, 02020
- see
- Ejectors
- see
- Double Lock Nuts
- see
- Statistics
- Calculation of Forces on Multi-Bar Planar Linkages, 90022
- equations and program for various types of four bar linkages, 90022
- Fatigue Strength
-
- see also
- Bolted Butt Joints with Cover Plates in Steels
- Bolted Double Lap Joints in Steels
- Bolted Doublers on Both Sides of Plate in Steels
- Bolted Joints
- Bonded Double-Strap Joints in Clad Aluminium Alloys
- Bonded Single-Lap Joints in Clad Aluminium Alloys
- Fretting Fatigue
- High-Load Transfer Joints in Aluminium Alloys
- Low-Load Transfer Joints in Aluminium Alloys
- Lugs (Fatigue Strength)
- Lugs (Stress Concentration Factors)
- Lugs (Stress Intensity Factors)
- Medium-Load Transfer Joints in Aluminium Alloys
- Nuts
- Riveted Lap Joints in Aluminium Alloy Sheets
- Screw Threads
- Studs
- Welded Attachments in Aluminium Alloys
- Welded Joints in Steels
- Welded Longitudinal Joints in Aluminium Alloys
- Welded Longitudinal Joints in Steels Under Axial Loading
- Welded Tee Joints in Aluminium Alloys
- Welded Transverse Joints in Aluminium Alloys
- Welded Transverse Joints in Steels Under Axial Loading
- Welded Transverse Joints in Steels Under Bending
- considerations in calculation under variable amplitude loading, 95006
- typical aircraft type in aluminium alloys, FAT E.05.01
- Fatigue Strength Under Acoustic Loading
- considerations in design for, 86025
- design of test specimens and test techniques under simulated loading, 93027
- Heat Conduction Across, 78029, 97019
- effect of pressure, 78029, 97019
- Strength Analysis
- Transmission of Vibrational Power Between Coupled Curved or Flat Plates
- efficiency for direct coupling or coupling through a beam, 98020
- see also
- Dry Rubbing Bearings
- Estimation of Equilibrium Temperature Rise
- Externally-Pressurised (Hydrostatic) With Capillary-Restrictor Control in Laminar Operation
- assessment of flow regime, 92026, 92037
- avoidance of cavitation, 92026, 92037
- bearing width to meet overload and stiffness requirements, 92026, 92037
- capillary and rectangular recess dimensions, 92026, 92037
- choice of supply pressure, 92026, 92037
- determination of possible bearing induced instability, 92026, 92037
- prediction of bearing temperature, 92026, 92037
- prediction of eccentricity, 92026, 92037
- prediction of lubricant flow rate, 92026, 92037
- prediction of power loss, 92026, 92037
- recommended diametral clearance, 92026, 92037
- Guide to Choice of Type
- from load, speed and environmental considerations, 65007
- Materials for Hydrodynamic for Industrial Machine Applications
- 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, 88018
- maximum operating temperature, 88018
- relative fatigue strength, 88018
- selection procedure to meet operating requirements, 88018
- Oil-Lubricated Hydrostatic
- sketch of typical variation of friction coefficient with load and speed, 89044
- Oil-Lubricated Pressure-Fed Hydrodynamic, Axial Grooves in Laminar Operation
- choice of bearing dimensions, 84031, 93005
- choice of groove dimensions, 84031, 93005
- design and analysis procedure, 84031
- linearised damping coefficients for use in rotor response and stability analysis, 95023
- linearised stiffness coefficients for use in rotor response and stability analysis, 95023
- maximum allowable temperature, 84031, 93005
- minimum allowable film thickness, 84031, 93005
- prediction of bearing maximum temperature, 84031, 93005
- prediction of eccentricity ratio and film thickness, 84031, 93005
- prediction of lubricant film effective temperature, 84031
- prediction of lubricant film maximum temperature, 84031, 93005
- prediction of lubricant flow rate and power loss, 84031, 93005
- prediction of non-laminar flow, 84031
- sketch of typical variation of friction coefficient with load and speed, 89044
- Prediction of Transition From Laminar to Superlaminar Operation, 85028
- Pressure-Fed Hydrodynamic, Axial Grooves in Superlaminar Operation
- prediction of bearing maximum temperature, 85028, 93005
- prediction of eccentricity ratio and film thickness, 85028, 93005
- prediction of lubricant film effective temperature, 85028
- prediction of lubricant film maximum temperature, 85028, 93005
- prediction of lubricant flow rate and power loss, 85028, 93005
- Pressure-Fed Hydrodynamic, Circumferential Groove in Laminar Operation
- bearing-induced instability, 90027, 93004
- choice of bearing dimensions, 90027, 93004
- choice of groove dimensions, 90027, 93004
- design and analysis procedure, 90027
- maximum allowable temperature, 90027, 93004
- minimum allowable film thickness, 90027, 93004
- prediction of bearing maximum temperature, 90027, 93004
- prediction of eccentricity ratio and film thickness, 90027, 93004
- prediction of lubricant film effective temperature, 90027
- prediction of lubricant film maximum temperature, 90027, 93004
- prediction of lubricant flow rate and power loss, 90027, 93004
- Process-Fluid Lubricated Pressure-Fed Hydrodynamic, Axial Grooves in Laminar/Superlaminar Operation
- choice of bearing dimensions, 84031, 85028, 93006
- choice of groove dimensions, 84031, 85028, 93006
- design procedure following Item No. 84031 or 85028, 86008
- linearised damping coefficients for use in rotor response and stability analysis, 95023
- linearised stiffness coefficients for use in rotor response and stability analysis, 95023
- material combinations for use with particular process fluids or water, 86008
- maximum allowable temperature, 84031, 85028, 93006
- minimum allowable film thickness, 84031, 85028, 93006
- minimum clearance ratio for initial design, 86008
- prediction of eccentricity ratio and film thickness, 84031, 85028, 93006
- prediction of lubricant film maximum temperature, 84031, 85028, 93006
- prediction of lubricant flow rate and power loss, 84031, 85028, 93006
- principal design considerations, 86008
- requirements for lubricant filtration, 86008
- Non-Linear Systems
- use of describing functions to predict, 84032