ESDU A-Z Index: B-BOIK
- Effect on Control Hinge Moment Derivatives With Deflection or Incidence
- example calculation, 89010
- general discussion, AERO C.04.01.00
- Irving internal in two-dimensional flow, AERO C.04.01.04
- nose in two-dimensional flow, AERO C.04.01.03
- shielded horn, 88003
- unshielded horn, 88003
- use of two-dimensional data for wing with part-span control, 89009
- use of two-dimensional data for wing with spanwise section variation, AERO C.04.01.06
- Approximate Estimation for Transport Aircraft
- effects of various levels of deceleration, 76011
- Approximate Estimation of Decision Speed Ratio, 76011
- Definition, 76011
- Detailed Example Calculation Procedure and Results for Typical Transport Aircraft
- 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
- Typical Values of Deceleration, 76011
- Effect of Frame and Link Elasticity on, 89043
- Effect on Braking Torque, 89043
- Effect on Starting Torque, 89043
- Hodograph as Aid to Selecting Method, 89043
- use as guide to pin forces, 89043
- Reasons for Eliminating or Reducing Shaking Forces and Moments, 89043
- Selection of Methods or Combination of Methods, 89043
- Various Methods to Eliminate or Reduce Shaking Forces or Moments
- comparison of advantages and limitations, 89043
- see
- Parachutes
- see
- Plug Valves
- Definition, 22001
- Measurement of Viscosity, 81002
- see also
- Boundary Walls and Fences
- Heat Transfer Along
-
- see
- Heat Transfer
- Stress Concentration in
- Estimation for Cylindrical Body at Zero Incidence in Supersonic Flow With Supersonic Jet
- discussion of effect of underexpanded jet on upstream separation, 99010
- effect of jet and freestream Mach numbers, 99010
- effect of jet exit angle, 99010
- effect of jet specific heat capacity ratio, 99010
- effect of jet to freestream total temperature ratio, 99010
- outline of flow model adopted, 99010
- practical ranges of variables affecting value, 99010
- Estimation for Truncated Conical Boat-Tail at Zero Incidence in Supersonic Flow With Supersonic Jet
- derived from base pressure on corresponding cylinder, 00017
- see also
- Base Pressure
- Aerofoils, AERO W.S.00.03.03, AERO W.S.02.03.07
- Bodies of Revolution
- brief discussion, AERO B.S.02.03.01
- Bodies of Revolution With Circular-Arc or Parabolic Boat-Tailing in Subsonic and Transonic Flow
- effect of base diameter, boat-tail angle and Mach number, 96012
- Bodies of Revolution With Conical Boat-Tailing in Subsonic, Transonic and Supersonic Flow
- development of correlation of experimental data using similarity laws, 98026
- discussion of quality of correlation of experimental data, 98026
- statistical assessment of accuracy of correlation of experimental data, 98026
- Bodies of Revolution With or Without Conical Boat-Tailing in Subsonic Flow
- effect of base diameter and boat-tail angle, 76033
- Bodies of Revolution With or Without Conical Boat-Tailing in Supersonic Flow
- effect of base diameter, boat-tail angle and Mach number, 79022
- Bodies of Revolution With or Without Conical Boat-Tailing in Transonic Flow
- effect of angle of attack, 96033
- effect of base diameter, boat-tail angle and Mach number, 78041
- Bodies of Revolution Without Boat-Tailing in Supersonic Flow
- effect of stabilising fins at or upstream of base, 97022
- laminar or turbulent boundary layer, AERO B.S.02.03.12
- Circular Cylinder in Subsonic, Transonic and Supersonic Flow
- development of correlation of experimental data using beta functions, 98026
- statistical assessment of accuracy of correlation of experimental data, 98026
- vacuum limit, 98026
- Flat Plate With Turbulent Boundary Layer
- guide to alleviation, 10017
- means of prediction, 10016
- Circular Plates Normal to Flow, 83020
- Finite Length Rectangular- and Square-Section Cylinders Normal to Flow, 71016
- surface-mounting effects, 71016
- Paraboloidal Antennas Aligned, Inclined or Normal to Flow, 83020
- Relationship With Base Drag, 76033
- Surface-Mounted Circular-Section Cylinders Normal to Flow, 81017
- Two-Dimensional Circular-Section Cylinders Normal to Flow, 80025
- Two-Dimensional Rectangular- and Square-Section Cylinders Normal to Flow, 71016
- Process Engineering
- application of process integration techniques to, 90033
- Description, 73004
- Guidance on Contribution to Aircraft Drag, 94044
- see also
- Beams of Angle Section
- Beams of Any Hollow or Solid Polygonal Section
- Beams of Box Construction
- Beams of Channel Section
- Beams of Circular Section
- Beams of I-Section
- Beams of Rectangular Tubular Section
- Beams of Sandwich Construction
- Beams of T-Section
- Beams of Unlipped Z-Section
- Cantilevers of Uniform Section
- Curved Beams
- Propped Cantilevers of Uniform Section
- Welded Cover Plates on Steel I-Beams
- Welded Joints in Steels
- Welded Longitudinal Joints in Aluminium Alloys
- Welded Longitudinal Joints in Steels Under Axial Loading
- Welded Stiffening Gussets on Steel I-Beams
- Welded Transverse Joints in Steels Under Axial Loading
- Welded Transverse Joints in Steels Under Bending
- Allowable Stresses, SS3
- Constant Section Encastre or Simply Supported
- bending moments, deflections and reactions for various loadings, SS3
- Constant Section Under Lateral Loading
- critical load for lateral instability, 88034
- Dynamic Response
- equation for modal density in bending, 99009
- Effect on Transmission of Vibrational Power When Used to Couple Plates
- prediction of efficiency for up to six curved or flat plates, 98020
- Factors of Safety, SS3
- Introduction to Crossflow Behaviour for Wind Loading Considerations, 71012
- Introduction to Inelastic Behaviour, 18001
- Introduction to Inelastic Behaviour, 18001
- Program to Predict Bending Moment Giving Maximum Allowable Inelastic Stress/Strain at Extreme Fibre
- inelastic form factors, 88035
- sections symmetrical about bending axis, 88035
- Section Characteristics
- area and moment of inertia, 91001
- Use of Constrained Single- or Multi-Layer Treatments on One Side
-
- see also
- Damping
- to increase structural damping, 91012, 91013
- Use of Free-Layer Treatments on One or Both Sides
-
- see also
- Damping
- to increase structural damping, 91012, 91013
- With Sectional Discontinuities and Any Support System
- deflections and slopes for any loading, 69017
- Programs to Predict Loads Giving Maximum Allowable Stress/Strain at Extreme Fibre
- elastic and inelastic analysis, 90004, 90026
- location of neutral axis, 90004, 90026
- outputs loads (end load, orthogonal bending moments) in same ratio as input, 90004
- outputs one load (out of end load, orthogonal bending moments) given other two, 90026
- radius of curvature of beam, 90004, 90026
- section area, centroid and second moment, 90004, 90026
- stresses and strains at cross-section vertices, 90004, 90026
- with beam constrained to deflect in one plane, 90004, 90026
- Estimation of Stresses Under Acoustic Loading, 74026
- Mean Forces and Pressures Due to Wind or Other Fluid Crossflow
- Natural Frequencies, 74025
- Rate of Change of Force With Wind Incidence, 93013
- Under Bending
- flange design for constant edge strain, STRUCT 02.05.00
- Form Factors for Inelastic Behaviour, 18002
- Mean Forces and Pressures Due to Wind or Other Fluid Crossflow
- Orthotropic (Laminated Composite) Faceplates (Specially-Orthotropic or Unbalanced)
- program for prediction of faceplate wrinkling, 87013
- Form Factors for Inelastic Behaviour, 18003
- Pressure Under Tyre Footprint on Wet Surface, TM 211
- see
- Ceramics
- Contact Phenomena
- Dry Rubbing Bearings
- Elastohydrodynamic Lubrication
- Flexure-Pivots
- Graphite
- Grease in Rolling Bearings
- Journal Bearings
- Porous Metal Bearings
- Rolling Bearings
- Rolling Bearings for Specialised Applications
- Self-Contained Bearing Assemblies
- Thrust Bearings
- Tribology Series
- Wear Resistant Surface Coatings and Treatments
- Values for Various Metallic Materials
- aluminium, copper and magnesium alloys, and nickel steels and steels 00932 (MMDH)
- see
- Disc Springs
- Calculation for Aircraft in Steady Level Asymmetric Manoeuvres
- on fin, fuselage, tailplane and wing, 01010
- Calculation for Aircraft in Steady Symmetric Manoeuvres
- fuselage and straight or swept medium to high aspect ratio wing, 94045
- Correlation of Wing Root With Wing Structure Weight, 98013
- Loading on Buildings and Structures Due to Atmospheric Turbulence
- across-wind component of turbulence, 89049, 92036
- along-wind component of turbulence, 87035, 88019, 92036
- Stress Analysis
- With Internal Flow
- design information for guide vanes, 83037
- Density and Dynamic and Kinematic Viscosity
- typical values in liquid state, 71003
- Definition and Discussion of Some Properties, 98026
- Aerodynamic Centre and Pitching Moment, AERO W.S.00.03.04
- Lift, AERO W.S.00.03.04
- Profile Drag, AERO W.S.02.04.13
- Wave Drag, AERO W.S.00.03.04
- Linear Systems
- definition, 67038
- Linear Systems
- definition, 67038
- Definition, 89022
- see
- Statistics
- Petroleum Products
- calculation of kinematic viscosity, 71003
- see
- Boundary Layer
- Description of Flow Around, 71012
- surface-mounted circular-section cylinders, 81017
- Dynamic Response to Turbulence and Wind
- Mean and Peak Forces, Moments and Pressures Due to Wind or Other Fluid Flows
-
- see
- Axial Force
- Base Pressure
- Boundary Walls and Fences
- Centre of Pressure
- Critical Conditions in Fluid Flow
- Derivatives
- Hoardings (Elevated Above Ground Level)
- Internal Pressure
- Normal Force
- Overturning Moment on Surface-Mounted Structures
- Pressure Distribution
- Profile Drag
- Rotational Moment
- Sideforce
- Torsional Moment on Structures
- Wind-Tunnel Testing
- Effect on Wave Drag of Flat Plates, AERO W.S.02.03.10
- see also
- Afterbody
- Aerodynamic Effects on Forebody-Cylinders at Subsonic, Transonic or Supersonic Speeds
- centre of pressure position at angles of attack to 90?, 87033, 90034
- normal force at angles of attack to 90?, 87033, 90034
- normal-force-curve slope at zero angle of attack, 87033
- pitching moment at angles of attack to 90?, 87033, 90034
- Cylinders of Rectangular-, Square- or Other Multi-Sided Section
-
- see
- Axial Force
- Base Pressure
- Bluff Bodies
- Centre of Pressure
- Critical Conditions in Fluid Flow
- Derivatives
- Internal Pressure
- Normal Force
- Overturning Moment on Surface-Mounted Structures
- Pitching Moment
- Pressure Distribution
- Profile Drag
- Response of Buildings and Structures
- Response of Buildings and Structures To Atmospheric Turbulence
- Response of Buildings and Structures To Vortex Shedding
- Sideforce
- Torsional Moment on Structures
- Elliptical Section
- tentative method for estimation of profile drag at zero incidence, 78019
- Surface Area of Streamlined Bodies of Rectangular Cross Section, 77028
- Volume, and Nose and Tail Angle or Radius of Curvature
- various nose and tail shapes with or without parallel mid body, 77028
- Boundary Layer Thickness and Shape Parameters
- variation with body geometry and flow conditions, 79020
- Circular Cylinders (With or Without Forebody or Afterbody)
-
- see
- Axial Force
- Base Drag (without Blowing or Jet Efflux)
- Base Drag with Central Propulsive Jet
- Base Pressure
- Bluff Bodies
- Boat-Tailing
- Boundary Layer
- Centre of Pressure
- Cone Cylinders
- Derivatives
- Ellipsoidal-Nosed Cylinders
- Equilibrium Surface Temperature
- Flow Separation
- Forced Convection Heat Transfer
- Forebody-Cylinders
- Free Convection Heat Transfer
- Internal Pressure
- Normal Force
- Ogive Cylinders
- Overturning Moment on Surface-Mounted Structures
- Pitching Moment
- Pressure Distribution
- Pressure Drag
- Profile Drag
- Response of Buildings and Structures
- Response of Buildings and Structures To Atmospheric Turbulence
- Response of Buildings and Structures To Vortex Shedding
- Sideforce
- Skin Friction Drag
- Drag at Supersonic Speed, AERO B.S.02.03.01
- Effect on Thrust and Drag of Interference With Pusher or Tractor Propeller Flow, 86017
- Estimation of Drag-Rise Mach Number, 74013
- Estimation of Upwash, 90020
- Goethert Compressibility Rule, 74013
- Planform Area and Its Centroid
- various nose and tail shapes with or without parallel mid body, 77028
- Profile Drag in Subcritical Flow at Zero Incidence
- estimation and effect of varying body geometry, 78019
- Similarity Laws Applied to Lift, Pitching Moment, Pressure and Pressure Drag Coefficients
- in subsonic or supersonic flow, 97025
- Surface Area and Volume, Nose and Tail Angle or Radius of Curvature
- various nose and tail shapes with or without parallel mid body, 77028
- Velocity Distribution in Subcritical Flow at Zero Incidence
- variation with body geometry and flow conditions, 78037
- Vortex Separation Points
- at angles of attack up to 60 degrees in supersonic flow, 91042