Drag (Chapter 7) Flashcards
Laminar flow changes to turbulent flow at the……………point
Transition point
The transition point shall never be:
Aft of the maximum thickness of the aerofoil
Laminar air flow has a ___________ velocity gradient
shallow
Turbulent airflow has a _____________ velocity gradient
Steep
The lowest pressure of an aerofoil is on the _______ of the aerofoil
Top
The separation point shall move __________ with an increase in AoA
Forwards
Laminar flow is:
Low Energy
Thin layer (1-2mm)
Predictable airflow
Turbulent airflow is:
High energy
Thick layer (2-3cm)
Mixed airflow
Reynolds Number is:
A dimensionless number which states the type of airflow (<500,00 is laminar) (>10,000,000 is turbulent)
Skin Friction drag
The drag which occurs within the boundary layer of the aerofoil
Form Drag
The drag which is created due to the pressure differential behind the trailing edge of the aerofoil