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FLIGHT MECHANICS
Presented by - Ganesh Natarajan S
Target Audience: Gate Aerospace, Aeronautical and Aerospace Engineering Students, etc.
SIDESLIP
β
V∞
CORE TOPICS
Basics: Atmosphere: Properties, standard atmosphere. Classification of aircraft. Airplane (fixed
wing aircraft) configuration and various parts. Pressure altitude; equivalent, calibrated, indicated
air speeds; Primary flight instruments: Altimeter, ASI, VSI, Turn-bank indicator. Angle of
attack, sideslip; Roll, pitch & yaw controls. Aerodynamic forces and moments.
Airplane performance: Drag polar; takeoff and landing; steady climb & descent; absolute and
service ceiling; range and endurance, load factor, turning flight, V-n diagram. Winds: head, tail
& cross winds.
Static stability: Stability & control derivatives; longitudinal stick fixed & free stability;
horizontal tail position and size; directional stability, vertical tail position and size; lateral
stability. Wing dihedral, sweep & position; hinge moments, stick forces.
SPECIAL TOPICS
Dynamic stability: Euler angles; Equations of motion; Decoupling of longitudinal and lateral-
directional dynamics; longitudinal modes; lateral-directional modes.
SYLLABUS
Outline
Let’s Start
SIDESLIP
Previous Lessons Angle of Attack
Slip
• Definition
• Types of Slip
Sideslip Angle (β)
• Definition
• Sideslip Angle (+Ve & -Ve)
• Restoring Yawing Moment
Sideslip
• Physical Significance
• Calculation & Measurement
Slip:
A slip is an aerodynamic state where an
aircraft is moving somewhat sideways as
well as forward relative to the oncoming
airflow or relative wind.
• Slip: Un-coordinated Flight.
Types of Slip
 Forward Slip: reduce height
 Sideslip: move the aircraft sideways
1. Crab method
2. Wing low method
Slip & its typesMotionImageryStandardsBoard(MISB)/Publicdomain
Sideslip Angle
Definition
The angle between the relative wind (V∞) and the
projection of the airplane’s longitudinal axis is known
as the sideslip angle
• The sideslip angle is symbolized as “ β ”.
• Co-ordinated Flight - zero sideslip angle.
β
V∞
RelativeHeadwind
Relative Crosswind
+ β
V∞
- β
V∞
Sideslip Angle
Positive Sideslip Angle
Negative Sideslip Angle
V∞
- N
V∞
Restoring Yawing Moment
Positive Yawing MomentNegative Yawing Moment
+ N
β = 0
Physical Significance: Crosswind landings
In crosswind conditions, the pilot is required to fly at a sideslip angle in order
to maintain alignment with the runway. [Transport airplanes ≤ 15.5 m/s]
Mysid/CCBY-SA(https://creativecommons.org/licenses/by-sa/3.0)
Calculation of Sideslip Angle
Y
Sideslip Angle Formula
β = sin-1 𝑣
𝑉
i.e. sinθ =
𝑂𝑝𝑝
𝐻𝑦𝑝
α = tan-1 𝑤
𝑢
i.e. tanθ =
𝑂𝑝𝑝
𝐴𝑑𝑗
Similarly
If the sideslip and angle of attack are smaller than. i.e. < 15°
β =
𝑣
𝑉
α =
𝑤
𝑢
Where V = (u2 + v2 +w2)1/2
*The value of α and β values are in radians*
The sideslip (β) and angle of attack (α) can be defined in
in terms of the velocity components, using trigonometry
FederalAviationAdministration/Publicdomain
Sideslip Measurement
Yaw String
Turn & Slip Indicator
Book Reference
• Flight stability and automatic control (2nd Edition), Dr. Robert C. Nelson;
Pg.No: (21 & 30).
• Pilot's handbook of aeronautical knowledge 2016 - Chapter 5: Aerodynamics
of flight (5-18) Pg No: (117/524)
SIDESLIP
Summary
Sideslip
β
Determination
Copyright Notice: Images used in this
presentation are sourced from pixabay.com
under “Pixabay License” which are “Free
for commercial use and No attribution
required” category (or) from other
sources, in which case appropriate
attributions are provided.
Sideslip | Flight Mechanics | GATE Aerospace

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Sideslip | Flight Mechanics | GATE Aerospace

  • 1. FLIGHT MECHANICS Presented by - Ganesh Natarajan S Target Audience: Gate Aerospace, Aeronautical and Aerospace Engineering Students, etc. SIDESLIP β V∞
  • 2. CORE TOPICS Basics: Atmosphere: Properties, standard atmosphere. Classification of aircraft. Airplane (fixed wing aircraft) configuration and various parts. Pressure altitude; equivalent, calibrated, indicated air speeds; Primary flight instruments: Altimeter, ASI, VSI, Turn-bank indicator. Angle of attack, sideslip; Roll, pitch & yaw controls. Aerodynamic forces and moments. Airplane performance: Drag polar; takeoff and landing; steady climb & descent; absolute and service ceiling; range and endurance, load factor, turning flight, V-n diagram. Winds: head, tail & cross winds. Static stability: Stability & control derivatives; longitudinal stick fixed & free stability; horizontal tail position and size; directional stability, vertical tail position and size; lateral stability. Wing dihedral, sweep & position; hinge moments, stick forces. SPECIAL TOPICS Dynamic stability: Euler angles; Equations of motion; Decoupling of longitudinal and lateral- directional dynamics; longitudinal modes; lateral-directional modes. SYLLABUS
  • 3. Outline Let’s Start SIDESLIP Previous Lessons Angle of Attack Slip • Definition • Types of Slip Sideslip Angle (β) • Definition • Sideslip Angle (+Ve & -Ve) • Restoring Yawing Moment Sideslip • Physical Significance • Calculation & Measurement
  • 4. Slip: A slip is an aerodynamic state where an aircraft is moving somewhat sideways as well as forward relative to the oncoming airflow or relative wind. • Slip: Un-coordinated Flight. Types of Slip  Forward Slip: reduce height  Sideslip: move the aircraft sideways 1. Crab method 2. Wing low method Slip & its typesMotionImageryStandardsBoard(MISB)/Publicdomain
  • 5. Sideslip Angle Definition The angle between the relative wind (V∞) and the projection of the airplane’s longitudinal axis is known as the sideslip angle • The sideslip angle is symbolized as “ β ”. • Co-ordinated Flight - zero sideslip angle. β V∞ RelativeHeadwind Relative Crosswind
  • 6. + β V∞ - β V∞ Sideslip Angle Positive Sideslip Angle Negative Sideslip Angle
  • 7. V∞ - N V∞ Restoring Yawing Moment Positive Yawing MomentNegative Yawing Moment + N β = 0
  • 8. Physical Significance: Crosswind landings In crosswind conditions, the pilot is required to fly at a sideslip angle in order to maintain alignment with the runway. [Transport airplanes ≤ 15.5 m/s] Mysid/CCBY-SA(https://creativecommons.org/licenses/by-sa/3.0)
  • 10. Sideslip Angle Formula β = sin-1 𝑣 𝑉 i.e. sinθ = 𝑂𝑝𝑝 𝐻𝑦𝑝 α = tan-1 𝑤 𝑢 i.e. tanθ = 𝑂𝑝𝑝 𝐴𝑑𝑗 Similarly If the sideslip and angle of attack are smaller than. i.e. < 15° β = 𝑣 𝑉 α = 𝑤 𝑢 Where V = (u2 + v2 +w2)1/2 *The value of α and β values are in radians* The sideslip (β) and angle of attack (α) can be defined in in terms of the velocity components, using trigonometry
  • 12. Book Reference • Flight stability and automatic control (2nd Edition), Dr. Robert C. Nelson; Pg.No: (21 & 30). • Pilot's handbook of aeronautical knowledge 2016 - Chapter 5: Aerodynamics of flight (5-18) Pg No: (117/524) SIDESLIP
  • 13. Summary Sideslip β Determination Copyright Notice: Images used in this presentation are sourced from pixabay.com under “Pixabay License” which are “Free for commercial use and No attribution required” category (or) from other sources, in which case appropriate attributions are provided.