ESDU A-Z Index: Y-YZ

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Yaw
Effect on Forces, Moments and Pressures on Bluff Bodies
see
Profile Drag
Sideforce
Effect on Ground Forces on Braked or Unbraked Rolling Aircraft Tyres
see also
Aircraft Tyres
incorporation in equations of motion, 85030
Rate
see
Yawing
Side-force Coefficients on Aircraft Tyres in Yawed and Unbraked Motion on Dry and Wet Pavements, 10002, 13007, 15007
Use of Damper to Control Dutch Roll, 83024
Yawing
see also
Derivatives
Moment
see also
Yawing Moment Due To Aileron Deflection (Nξ or CnΔa)
Yawing Moment Due To Rolling (Np or Cnp)
Yawing Moment Due To Rudder Deflection (Nζ or CnΔr)
Yawing Moment Due To Sideslip (Nv or Cnβ)
Yawing Moment Due To Spoiler Deflection
Yawing Moment Due To Yawing (Nr or Cnr)
information on the use of Data Items on yawing moment and sideforce derivatives of an aircraft, AERO A.07.01.00
on single- or contra-rotating propellers due to angle of attack at low forward speeds, 89047
Rolling Moment Due to
see
Rolling Moment Due To Yawing (Lr or Clr)
Yawing Moment Due To Aileron Deflection (Nξ or CnΔa)
Estimation From Induced Drag and Profile Drag Contributions, 88029, 88040
Yawing Moment Due To Rolling (Np or Cnp)
Use for Complete Aircraft of Data Items on Component Contributions
accuracy, 85010
comparison of experimental and predicted variation with incidence, 85010
examples, 85010
Wing (With Zero Camber and Twist) Contribution
attached and separated flow, 81014
compressibility effects, 81014
discussion of edge forces, 81014
effect of dihedral, 85006
Yawing Moment Due to Rolling, AERO A.07.01.00
Yawing Moment Due To Rudder Deflection (Nζ or CnΔr)
Estimation at Low Speeds
from geometry of rear fuselage and empennage, 87008
Yawing Moment Due To Sideslip (Nv or Cnβ)
Estimation for Wing-Body Combination, 00025, 79006
Fin Contribution
single fin (fuselage height/width near one), 00025, 82010
single fin merging into fuselage, AERO C.01.01.01
single or twin fins at supersonic speeds, 91031
single or twin fins (range of fuselage height/width), 93007
tailplane-mounted twin fins, 92007
Flap Contribution, 00025, 81013
Nacelle Contribution (Propeller Type) on Wing, 00025, TM 178
Nacelle Contribution (Turbine Engine Type)
rear-fuselage mounted/empennage interference, 73006
underwing mounted, 00025, 73006
Program to Calculate for Complete Aircraft, 00025
Tailplane Effects, 00025, 81032, 82010, 93007
Use for Complete Aircraft of Data Items on Component Contributions
accuracy, 82011
examples, 00025, 82011
Ventral Fin Contribution
single or twin at subsonic or supersonic speeds, 92029
Yawing Moment Due to Sideslip, AERO A.07.01.00
Yawing Moment Due To Spoiler Deflection
Estimation When Perforated or Solid is Used as Roll Control
including contributions from spoiler-wake-fin and flap-spoiler interference, 96026
Yawing Moment Due To Yawing (Nr or Cnr)
Body Contribution, 83026
Fin and Tailplane Combined Contribution, 83006
Fin Contribution, 82017
Simplified Method of Estimation, 84002
Use for Complete Aircraft of Data Items on Component Contributions
accuracy, 84002
comparison of experimental and predicted variation with incidence, 84002
example, 84002
Wing Contribution
attached flow, 71017
bibliography for separated flow, 71017
Yawing Moment Due to Yawing, AERO A.07.01.00
Y-Force
see
Derivatives
Sideforce
Yielding
Criteria for Ductile Materials
three-dimensional stress system, 73004
two-dimensional stress system, 73004, STRUCT 02.00.00
Description of Process, 73004
Yield-Pseudoplastic Fluid
see
Non-Newtonian Fluids
Y-Junctions in Ducts
see
Pressure Drop in Internal Flow
Young's Modulus
see also
Adhesives for Bonded Joints
Aluminium Alloys
Copper Alloys
Magnesium Alloys
Nickel Steels
Steels
Titanium Alloys
Effective Values for Components in Contact, 85027, 89045, 94017
Values for Various Ceramic Materials, 78035, 84041, 85027
Values for Various Metallic and Polymer Materials, 78035, 84041, 85027, 94017, 96002
Values for Various Piping Materials, 83046, 87027
Y-Valves
Pressure Drop Across, 69022

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