Sideslip | Flight Mechanics | GATE Aerospace

1,518 views 14 slides Aug 25, 2020
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About This Presentation

For Video Lecture of this presentation: https://youtu.be/u7bp9IJqRVM

The topics covered in this session are, Slip: Types of slip, Sideslip angle, Sideslip angle sign conventions, restoring yaw moments, physical significance, Calculation of sideslip angle, Measurement of sideslip.

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Slide Content

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

SIDESLIP

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 Crab method Wing low method Slip & its types Motion Imagery Standards Board (MISB) / Public domain

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 ∞ Relative Headwind Relative Crosswind Relative Wind

+ β V ∞ - β V ∞ Sideslip Angle Positive Sideslip Angle Negative Sideslip Angle

V ∞ - N V ∞ Restoring Yawing Moment Positive Yawing Moment Negative 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 / CC BY-SA (https://creativecommons.org/licenses/by-sa/3.0)

Calculation of Sideslip Angle Y

Sideslip Angle Formula β = sin -1   i.e. sin θ =   α = tan -1   i.e. tan θ =   Similarly If the sideslip and angle of attack are smaller than. i.e. < 15° β =   α =   Where V = (u 2 + v 2 +w 2 ) 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

Federal Aviation Administration / Public domain Sideslip Measurement Yaw String Turn & Slip Indicator

Book Reference Flight stability and automatic control (2 nd 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

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.