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Aeronautical Engineering
S/EN/18. Boundary Layers, Flat Plate Flow, Wing Planforms and Normal Shock Waves
- WORDS:
- 2900
- DATE:
- 2003
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- 29.99 GBP
This assignment covers basic laws and theories involved with aerodynamics from basic to more advanced levels. The topics covered include boundary layers, shock waves, horse shoe vortices, wing planforms and thermodynamic laws. These areas are addressed by the answering of questions set in the assignment sheets at the back of this assignment.
KEYWORDS: en, boundary, layers, flat, plate, flow, wing, planforms, normal, shock, waves,
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Keywords Tag Cloud
en design wing pressure flow aircraft engines applications waves planforms normal shock reliability piston gas aerodynamics lift flap speed low thermodynamics turbine cycles engineering layers operational features axial selection material fuselage preliminary review compressor coefficient boundary e flat cylinder circular drag distribution plate
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