ESDU A-Z Index: FIL-FLAS
- Fatigue Strength Improvement of Steel
- by surface rolling, 89031
- Under Torsion
- stress concentration factors, 75033
- Transformation of Analogue to Digital, 92044
- Use in Control System Design, 80018, 88039
- Use in Lubricant Circulation Systems
- definition of absolute and nominal rating, 83030
- factors determining choice of rating, 83030
- nominal ratings appropriate to various types of equipment, 83030
- Use to Control Particulate Fouling, 88024
- Applied to Estimation of Response to Excitation of Lightweight Structures
- advantages, features and limitations, 97033
- comparison of results for simple structure with those from statistical energy analysis, 99009
- outline of mathematical modelling, 97033
- typical applications, 97033
- Stiffnesses of Local Structural Details for Use With
- Aircraft
- Calculation of Bending Moment, Loading and Torque on in Steady Level Asymmetric Flight
- sideslipping, turning or with failed engine, 01010
- Effect on Base Drag of Cylindrical Afterbodies at Supersonic Speeds
- mounted at or upstream of base, 97022
- Profile Drag Increment in Turbulent Boundary Layer
-
- see
- Excrescences
- Trapezoidal- or Triangular-Section in Straight Pipes
- Viscous Full-potential (VFP) Method for Three Dimensional Wings and Wing-body Combinations
- estimation of excrescence drag at subsonic speeds and analysis program, 23013
- see also
- Dynamic Stability
- Linear Systems
- see
- Statistics
- see
- Propellers
- see also
- Joints
- Equipment to Aircraft Structures
- considerations in design against fatigue, 86025
- Effect on Buckling in Shear of Square Plates
- Stress Concentration Data
- see
- Curved Beams
- Choice of Optimum Deflections Using Multivariate Search and CFD Codes
- example studies for single design point, 00022, 00023, 99020
- example study together with camber line shape for two design points, 99021
- example study together with surface shape for two design points, 01024
- Contribution to Average Downwash at Tailplane in Attached Flow
- effect of compressibility, 97021
- effects of flap, tail and wing geometry, 97021
- Contribution to Rolling Moment Due to Sideslip, 00025, 80034
- effect with propeller slipstream, 06012
- Contribution to Rolling Moment Due to Yawing, 72021
- Contribution to Sideforce and Yawing Moment Due to Sideslip, 00025, 81013
- Contribution to Yawing Moment Due to Yawing, 71017
- Derivation of Part-Span Factors, TM 172
- Discussion of Regions of Supersonic Flow Occurring at Low Freestream Mach Numbers, 90008
- Drag Increment Due to Chord- or Spanwise Sealed/Unsealed Gaps for Undeflected at Low Speeds, 92039
- example of calculation including effect of faulty sealing, 93032
- Estimation of Nacelle and Flap Effects on Low-Speed Aerodynamic Centre and Zero-Lift Pitching Moment of Transport Aircraft (Tail-Off), TM 200
- Fowler
- normal force, AERO F.05.01.01
- Introduction to Data Items on Effect on Drag, Lift and Pitching Moment
- aerofoils, 94026
- wings, 97002
- Kruger With or Without Vent
- angle of attack for maximum lift of aerofoils or wings, 96003
- effect on lift of wing at zero angle of attack, 96032, 97002
- effect on maximum lift of basic aerofoil and its lift at zero angle of attack, 94027
- effect on maximum lift of wings, 92031
- effect on pitching moment of basic aerofoil and wing at zero angle of attack, 00029
- lift curve from zero to maximum lift of aerofoils or wings, 96003
- program to predict lift curve with deflected, 99031
- Kruger With or Without Vent in Combination With Trailing-Edge Flaps
- angle of attack for maximum lift of aerofoils or wings, 96003
- effect on lift of wing at zero angle of attack, 93019, 95021, 96032, 97002, 97009, 97011
- effect on maximum lift of basic aerofoil and its lift at zero angle of attack, 94027, 94028, 94029, 94031
- effect on maximum lift of wings, 91014, 92031
- lift curve from zero to maximum lift of aerofoils or wings, 96003
- program to predict lift curve with deflected, 99031
- Leading-Edge With Slot
- contribution to airframe noise, 90023
- Multi-Slotted
- angle of attack for maximum lift of aerofoils or wings, 96003
- contribution to airframe noise, 90023
- effect on lift of wing at zero angle of attack, 95021, 97002
- effect on maximum lift of basic aerofoil and its lift at zero angle of attack, 94031
- effect on maximum lift of wings, 91014
- effect on pitching moment of basic aerofoil and wing at zero angle of attack, 99014
- effect on trailing vortex drag of cambered and twisted or plane wings, 01007
- lift curve from zero to maximum lift of aerofoils or wings, 96003
- program to predict lift curve with deflected, 99031
- Multi-Slotted in Combination With Leading-Edge High-Lift Devices
- angle of attack for maximum lift of aerofoils or wings, 96003
- effect on lift of wing at zero angle of attack, 95021, 96032, 97002
- effect on maximum lift of basic aerofoil and its lift at zero angle of attack, 94027, 94031
- effect on maximum lift of wings, 91014, 92031
- lift curve from zero to maximum lift of aerofoils or wings, 96003
- program to predict lift curve with deflected, 99031
- Part-Span
- angle of attack for maximum lift of aerofoils or wings, 96003
- derivation of equations for profile drag increment conversion factors for part-span flaps, TM 216
- effect on lift of wing at zero angle of attack, 96032
- effect on maximum lift of wings, 91014
- lift curve from zero to maximum lift of aerofoils or wings, 96003
- lift increment from that due to full-span leading-edge high-lift devices, 96032
- lift increment from that due to full-span multi-slotted, 95021
- lift increment from that due to full-span plain, 97011
- lift increment from that due to full-span single-slotted, 93019
- lift increment from that due to full-span split, 97009
- profile drag increment from that due to full span, AERO F.02.01.07
- program to predict lift curve with deflected, 99031
- trailing vortex drag, AERO F.02.01.08
- Plain
-
- see also
- Hinge Moment
- angle of attack for maximum lift of aerofoils or wings, 96003
- effect of deflection of leading- and/or trailing-edge on wing loading distribution, 95010
- effect on lift of wing at zero angle of attack, 97002, 97011
- effect on maximum lift of basic aerofoil and its lift at zero angle of attack, 94028
- effect on maximum lift of wings, 91014
- effect on pitching moment of basic aerofoil and wing at zero angle of attack, 98017
- effect on profile drag of wings, 06014, 87024, AERO F.02.01.07
- effect on trailing vortex drag of cambered and twisted or plane wings, 01007
- lift curve from zero to maximum lift of aerofoils or wings, 96003
- normal force, AERO F.05.01.01
- program to predict lift curve with deflected, 99031
- Plain in Combination With Leading-Edge High-Lift Devices
- angle of attack for maximum lift of aerofoils or wings, 96003
- effect on lift of wing at zero angle of attack, 96032, 97002, 97011
- effect on maximum lift of basic aerofoil and its lift at zero angle of attack, 94027, 94028
- effect on maximum lift of wings, 91014, 92031
- lift curve from zero to maximum lift of aerofoils or wings, 96003
- program to predict lift curve with deflected, 99031
- Plain in Combination With Plain Leading-Edge Flaps
- effect on wing loading distribution, 95010
- Plain in Combination With Plain Leading-Edge Flaps (Both With Sealed Gaps)
- effect on drag, hinge and pitching moments, lift and pressure distribution using VGK, 01033
- effect on drag in viscous subsonic or transonic flow using VGK, 96028, 96029
- Profile Drag Due to Deployment of All Types on Wings
- derivation of equations for profile drag increment conversion factors for part-span flaps, TM 216
- increment due to part-span from known value for full-span, AERO F.02.01.07
- Single-Slotted
- angle of attack for maximum lift of aerofoils or wings, 96003
- contribution to airframe noise, 90023
- effect on lift of wing at zero angle of attack, 93019, 97002
- effect on maximum lift of basic aerofoil and its lift at zero angle of attack, 94030
- effect on maximum lift of wings, 91014
- effect on pitching moment of basic aerofoil and wing at zero angle of attack, 99004
- effect on profile drag of NACA and Handley Page types on wings, AERO F.02.01.06, AERO F.02.01.07
- effect on profile drag of optimum geometry on aerofoils, 87005
- effect on profile drag of optimum geometry on wing, 08013
- effect on trailing vortex drag of cambered and twisted or plane wings, 01007
- lift curve from zero to maximum lift of aerofoils or wings, 96003
- normal force, AERO F.05.01.01
- program to predict lift curve with deflected, 99031
- Single-Slotted in Combination With Leading-Edge High-Lift Devices
- angle of attack for maximum lift of aerofoils or wings, 96003
- effect on lift of wing at zero angle of attack, 93019, 96032, 97002
- effect on maximum lift of basic aerofoil and its lift at zero angle of attack, 94027, 94030
- effect on maximum lift of wings, 91014, 92031
- lift curve from zero to maximum lift of aerofoils or wings, 96003
- program to predict lift curve with deflected, 99031
- Slats or Sealed Slats
- angle of attack for maximum lift of aerofoils or wings, 96003
- effect on lift of wing at zero angle of attack, 96032, 97002
- effect on maximum lift of basic aerofoil and its lift at zero angle of attack, 94027
- effect on maximum lift of wings, 92031
- effect on pitching moment of basic aerofoil and wing at zero angle of attack, 00029
- lift curve from zero to maximum lift of aerofoils or wings, 96003
- program to predict lift curve with deflected, 99031
- Slats or Sealed Slats in Combination With Trailing-Edge Flaps
- angle of attack for maximum lift of aerofoils or wings, 96003
- effect on lift of wing at zero angle of attack, 93019, 95021, 96032, 97002, 97009, 97011
- effect on maximum lift of basic aerofoil and its lift at zero angle of attack, 94027, 94028, 94029, 94030, 94031
- effect on maximum lift of wings, 91014, 92031
- lift curve from zero to maximum lift of aerofoils or wings, 96003
- program to predict lift curve with deflected, 99031
- Split
- angle of attack for maximum lift of aerofoils or wings, 96003
- effect on lift of wing at zero angle of attack, 97002, 97009
- effect on maximum lift of basic aerofoil and its lift at zero angle of attack, 94029
- effect on maximum lift of wings, 91014
- effect on pitching moment of basic aerofoil and wing at zero angle of attack, 98009
- effect on profile drag of wings, 74010, AERO F.02.01.07
- effect on trailing vortex drag of cambered and twisted or plane wings, 01007
- lift curve from zero to maximum lift of aerofoils or wings, 96003
- normal force, AERO F.05.01.01
- program to predict lift curve with deflected, 99031
- Split in Combination With Leading-Edge High-Lift Devices
- angle of attack for maximum lift of aerofoils or wings, 96003
- effect on lift of wing at zero angle of attack, 96032, 97002, 97009
- effect on maximum lift of basic aerofoil and its lift at zero angle of attack, 94027, 94029
- effect on maximum lift of wings, 91014, 92031
- lift curve from zero to maximum lift of aerofoils or wings, 96003
- program to predict lift curve with deflected, 99031
- Split With Flap Trailing Edge Forward of Wing Trailing Edge When Undeployed
- pitching moment increment on swept wings, AERO F.08.01.02
- pitching moment increment on unswept wings, AERO F.08.01.01
- Trailing Vortex Drag Due to Deployment of All Types 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
- Approximate Method of Calculating Effect on Pressure Drop
- two-phase gas- or vapour-liquid flow through pipe fittings, 89012
- In Cam/Follower Lubricant Film
- prediction thoughout complete rotation, 00015