Aerodynamics at LMU München

Flashcards and summaries for Aerodynamics at the LMU München

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Study with flashcards and summaries for the course Aerodynamics at the LMU München

Exemplary flashcards for Aerodynamics at the LMU München on StudySmarter:

How does rotor downwash affect a helicopter with horizontal stabilizers (mounted at the tailboom) in a free air hover?

Exemplary flashcards for Aerodynamics at the LMU München on StudySmarter:

When the cyclic stick is pushed forward, a main rotor blade will reach its maximum blade pitch angle:

Exemplary flashcards for Aerodynamics at the LMU München on StudySmarter:

When the cyclic stick is pushed forward, a main rotor blade will reach its maximum blade pitch angle:

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Exemplary flashcards for Aerodynamics at the LMU München on StudySmarter:

That point where airflow leaves the surface of an aerofoil is known as:

Exemplary flashcards for Aerodynamics at the LMU München on StudySmarter:

Yawing in a helicopter is the term used to define a rotation:

Exemplary flashcards for Aerodynamics at the LMU München on StudySmarter:

The chord line of an airfoil section is the line:

Exemplary flashcards for Aerodynamics at the LMU München on StudySmarter:

The total rotor thrust is:

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Exemplary flashcards for Aerodynamics at the LMU München on StudySmarter:

In a hovering helicopter, recirculated air at the main rotor blade tips will cause:

Exemplary flashcards for Aerodynamics at the LMU München on StudySmarter:

If the collective pitch lever is lowered during straight and level flight the helicopter will pitch (1) because (2)

Exemplary flashcards for Aerodynamics at the LMU München on StudySmarter:

The center of pressure of an airfoil element:

Exemplary flashcards for Aerodynamics at the LMU München on StudySmarter:

The resultant force from pressure envelopes around an aerofoil can be described as:

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The lift coefficient of an airfoil section:

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Exemplary flashcards for Aerodynamics at the LMU München on StudySmarter:

Aerodynamics

How does rotor downwash affect a helicopter with horizontal stabilizers (mounted at the tailboom) in a free air hover?

it will pitch nose down.

Aerodynamics

When the cyclic stick is pushed forward, a main rotor blade will reach its maximum blade pitch angle:

on the retreating side.

Aerodynamics

When the cyclic stick is pushed forward, a main rotor blade will reach its maximum blade pitch angle:

on the retreating side.

Aerodynamics

That point where airflow leaves the surface of an aerofoil is known as:

the separation point

Aerodynamics

Yawing in a helicopter is the term used to define a rotation:

about the vertical axis.

Aerodynamics

The chord line of an airfoil section is the line:

drawn between the leading and the trailing edges.

Aerodynamics

The total rotor thrust is:

a force acting at right angles perpendicular to the relative air flow.

Aerodynamics

In a hovering helicopter, recirculated air at the main rotor blade tips will cause:

increased lift.

Aerodynamics

If the collective pitch lever is lowered during straight and level flight the helicopter will pitch (1) because (2)

(1) down (2) the coning angle decreases

Aerodynamics

The center of pressure of an airfoil element:

depends on the height of the airfoil element.

Aerodynamics

The resultant force from pressure envelopes around an aerofoil can be described as:

the total reaction

Aerodynamics

The lift coefficient of an airfoil section:

changes with the velocity of the airflow, squared.

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