2010Unpublished venueRequires access

Drag

P. J. Swatton

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Abstract

This chapter contains sections titled: Parasite (Profile) Drag Surface-Friction Drag Form (Pressure) Drag Induced Drag Ground Effect Wing-Tip Design Wingspan Loading The Coefficient of Induced Drag (CDI) Total Drag Analysis of the Total-Drag Curve The Velocity of Minimum Drag (VIMD) The Velocity of Minimum Power (VIMP) The Maximum EAS/Drag Ratio (VI/Dmax) Speed Speed Stability and Instability The Effect of the Variables on Total Drag The CL V CD Polar Diagram Analysis of the Lift/Drag Ratio Drag Augmentation Airbrakes Spoilers Barn-Door Flaps Drag Parachutes Self-Assessment Exercise 7

About this research paper

What this paper is about

This chapter contains sections titled: Parasite (Profile) Drag Surface-Friction Drag Form (Pressure) Drag Induced Drag Ground Effect Wing-Tip Design Wingspan Loading The Coefficient of Induced Drag (CDI) Total Drag Analysis of the Total-Drag Curve The Velocity of Minimum Drag (VIMD) The Velocity of Minimum Power (VIMP) The Maximum EAS/Drag Ratio (VI/Dmax) Speed Speed Stability and Instability The Effect of the Variables on Total Drag The CL V CD Polar Diagram Analysis of the Lift/Drag Ratio Drag Augmentation Airbrakes Spoilers Barn-Door Flaps Drag Parachutes Self-Assessment Exercise 7

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Available abstract

This chapter contains sections titled: Parasite (Profile) Drag Surface-Friction Drag Form (Pressure) Drag Induced Drag Ground Effect Wing-Tip Design Wingspan Loading The Coefficient of Induced Drag (CDI) Total Drag Analysis of the Total-Drag Curve The Velocity of Minimum Drag (VIMD) The Velocity of Minimum Power (VIMP) The Maximum EAS/Drag Ratio (VI/Dmax) Speed Speed Stability and Instability The Effect of the Variables on Total Drag The CL V CD Polar Diagram Analysis of the Lift/Drag Ratio Drag Augmentation Airbrakes Spoilers Barn-Door Flaps Drag Parachutes Self-Assessment Exercise 7

Key concepts: Drag, Zero-lift drag coefficient, Lift-induced drag, Parasitic drag, Drag coefficient, Drag divergence Mach number, Aerodynamic drag, Lift-to-drag ratio

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