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Introduction to Aerodynamics
Jun 28, 2024
Introduction to Aerodynamics
Definition and Scope
Aerodynamics
: Study of forces and moments on bodies moving through fluids, primarily air.
Key Focus
: Forces and moments (pressure, viscous stress) on the surface of bodies like aircraft.
Goal
: Determination of pressure and viscous stresses to predict motion of the body.
Aircraft Forces in Aerodynamics
Forces on Aircraft
: Lift, Drag, Weight, Thrust (Buoyancy force negligible)
Straight Level Flight
: Weight balanced by Lift, Thrust balanced by Drag.
Coordinate System for Forces and Moments
X-axis
: Along the relative wind (direction opposite to the aircraft's speed).
Y-axis
: Perpendicular to plane formed by X and Z axis; positive towards the starboard (right-wing) side.
Z-axis
: Normal to X-axis; upward but not vertical.
Components of Forces
Drag
: Along the relative wind (X-axis)
Lift
: Normal to the relative wind (not vertical)
Side Force
: In Y-direction; positive if towards the starboard
Moments on the Aircraft
Pitching Moment
: About Y-axis (raises/lowers the aircraft nose)
Rolling Moment
: About X-axis (one wing up, other down)
Yawing Moment
: About Z-axis (nose left or right)
Flight Dynamics
Assumption: Body (aircraft) is at rest, fluid (air) moves.
Forces in Symmetric Flight
: Primarily Lift, Drag, and Pitching Moment.
Aircraft Components
Key Components
: Fuselage, Wings, Horizontal Tail, Vertical Tail, Engine.
Functionality
:
Fuselage
: Main body housing passengers/cargo.
Wing
: Major lift generator (95% of total lift).
Wing Geometry and Parameters
Planform
: Shape of wing in plan view (e.g., trapezoidal, delta-wing).
Wingspan
: Distance from wingtip to wingtip.
Wing Area
: Planform area extended to the center of fuselage.
Aspect Ratio (AR)
: Span^2 / Wing Area
Chord
: Distance from leading edge to trailing edge of the wing section.
Taper Ratio
: Tip chord length / Root chord length
Sweep Angle and Twist
Sweep Angle
: Angle between Y-direction and leading/trailing edge.
Twist
: Change in chord plane across wing span affecting angle of attack at different sections.
Dihedral/Anhedral
: Wing tips above/below root in front view.
Airfoil Characteristics
Airfoil
: Cross-section shape of the wing.
Important Terms
:
Chord Line
: Line from leading edge to trailing edge.
Thickness
: Distance between upper and lower surfaces at any chord location.
Aspect Ratio
: Relative measure of wing slenderness.
Camber Line
: Line joining midpoints of thickness along chord.
Angle of Attack
: Angle between relative wind and chord line.
Designations
: Symmetric (no camber) vs. Cambered (curved mean line)
Summary
Understanding of basic aerodynamic concepts and aircraft components necessary.
Definitions and terms introduced form the foundation for further study in aerodynamics.
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