Exam 1 Flashcards

1
Q

Stream lines

A

Lines that indicate how air flows around an air foil

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2
Q

Lines that indicate how air flows around an air foil

A

Stream - lines

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3
Q

Stream tube

A

collection of stream lines

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4
Q

collection of stream lines

A

Stream tube

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5
Q

Stagnation stream lines

A

lines that terminate at or originate from an airfoil

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6
Q

lines that terminate at or originate from an airfoil

A

Stagnation stream lines

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7
Q

Continuity equation

A

ρAV = ρ’A’V’

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8
Q

ρAV = ρ’A’V’

A

Continuity equation

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9
Q

Bernoulli’s Equation

A

P+0.5ρV^2 =P’+0.5* ρ*V’^2=Po

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10
Q

P+0.5ρV^2 =P’+0.5* ρ*V’^2=Po

A

Bernoulli’s Equation

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11
Q

What does the equation ΔP=0.5ρV^2 demonstrate?

A

static pressure is always equal to dynamic pressure

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12
Q

What are the two fluid flow types?

A

Compressible and Incompressible

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13
Q

Compressible Flow

A

Flow in which the density of a fluid can change from point to point

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14
Q

Incompressible Flow

A

Flow in which the density of a fluid remains constant

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15
Q

Flow in which the density of a fluid remains constant

A

Incompressible Flow

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16
Q

Flow in which the density of a fluid can change from point to point

A

Compressible Flow

17
Q

Name the four forces acting on an aircraft in the air

A

1) Thrust
2) Lift
3) Drag
4) Weight

18
Q

What two forces acting on an aircraft are concerned with aerodynamics

A

1) Lift

2) Drag

19
Q

What are the 2 basic sources of an aerodynamic force?

A

1) Pressure

2) Frictional shear stress

20
Q

Pressure acts _____ to a surface, shear stress acts ____ to a surface

A

perpendicular; tangentially

21
Q

What are the four fundamental properties of a flowing gas (a.k.a. - the 4 properties of a flow field)?

A

1) Pressure (P)
2) Density (ρ)
3) Temperature (T)
4) Velocity (V)

22
Q

Equation of state

A

P = ρRT