Aerodynamic theories

Post on 06-May-2015

848 views 3 download

Transcript of Aerodynamic theories

Definition - ‘Force’ Definition – ‘Aerodynamic Force’ Fundamental sources of

Aerodynamic Force Pressure Distribution Shear Stress Types of Flows

Equation of Continuity Bernoulli’s Theorem / Application Flat Plate Effect

Aerodynamic TheoriesAerodynamic Theories 11

Definitions ‘Force’ ‘Aerodynamic Force’

Fundamental sources of Aerodynamic Force Pressure Distribution Shear Stress Types of Flows Equation of Continuity Bernoulli’s Theorem / Application Flat Plate Effect Conclusion

Aerodynamic TheoriesAerodynamic Theories 44

Aerodynamic TheoriesAerodynamic Theories 55

Introduction: Aerodynamics Basics

F16 pushes the F16 pushes the ground by 28000 lbs ground by 28000 lbs

and the ground and the ground pushes the a/c by pushes the a/c by

28000 lbs28000 lbs

Aerodynamic TheoriesAerodynamic Theories 88

Contact force / Surface force

Distance force / Body force

Aerodynamic TheoriesAerodynamic Theories 99

Frictional Force

Tensional Force

Air Resistance Force

Applied Force

Spring Force

Aerodynamic TheoriesAerodynamic Theories 1010

Aerodynamic TheoriesAerodynamic Theories 1111

Gravitational Force

Electrical Force

Magnetic Force

Aerodynamic TheoriesAerodynamic Theories 1212

Vector =Magnitude + Direction

350 Kts350 KtsHeading 345°Heading 345°

Aerodynamic TheoriesAerodynamic Theories 1313

Balanced force

Unbalanced force

Aerodynamic TheoriesAerodynamic Theories 1414

Force exerted on a body whenever there is a

relative velocity between the body and the

air

Aerodynamic TheoriesAerodynamic Theories 1616

Pressure Distribution

Shear Stress

Aerodynamic TheoriesAerodynamic Theories 1717

Aerodynamic TheoriesAerodynamic Theories 1818

1919Aerodynamic TheoriesAerodynamic Theories

Aerodynamic TheoriesAerodynamic Theories 2020

Pressure

Density

Temperature

Flow Velocity and Streamlines

Aerodynamic TheoriesAerodynamic Theories 2121

Speed and direction of gas may vary from point to point in the flow

The velocity at any fixed point B in a flowing gas is the velocity of an infinitesimally small fluid element as it sweeps through B

Aerodynamic TheoriesAerodynamic Theories 2222

Steady Streamline

Two Dimensional

Three Dimensional

Aerodynamic TheoriesAerodynamic Theories 2323

Flow parameters (speed, direction, pressure

variable)

May vary from point to point in the flow but

At any point are constant with respect to time

Classical Linear: More or less, streamlines follow

body contour without separation

Controlled Separated / LE Vortex Flow (at Hi

AOA) LE vortex on highly swept plan-forms, and

A strong controlled vortex (at a sharp LE) is made to produce

useful lift forceAerodynamic TheoriesAerodynamic Theories 2424

Aerodynamic TheoriesAerodynamic Theories 2525

Aerodynamic TheoriesAerodynamic Theories 2626