ESDU A-Z Index: Y-YZ
- Effect on Forces, Moments and Pressures on Bluff Bodies
- 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
- see also
- Derivatives
- Moment
- 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
- 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
- Estimation at Low Speeds
- from geometry of rear fuselage and empennage, 87008
- 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
- Estimation When Perforated or Solid is Used as Roll Control
- including contributions from spoiler-wake-fin and flap-spoiler interference, 96026
- 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
- see
- Derivatives
- Sideforce
- Criteria for Ductile Materials
- three-dimensional stress system, 73004
- two-dimensional stress system, 73004, STRUCT 02.00.00
- Description of Process, 73004
- Pressure Drop Across, 69022