para kay col8 Flashcards

(63 cards)

1
Q

balances should be ___ & ____

A

accurate and reliable

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2
Q

things to consider in 3d balance calibration

A

body axes, wind axes, wind axis components, velocity

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3
Q

types of body axes

A

lateral, longitudinal, vertical

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4
Q

3 types of forces in body axes

A

drag, lift, side force

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5
Q

6 COMPONENT BALANCE

A

Lift (L), Drag (D), Side Force (Y), Rolling Moment (l), Yawing Moment (n) , Pitching Moment (m)

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6
Q

LIFT FORMULA

A

C+D+E

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7
Q

DRAG FORMULA

A

A+B

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8
Q

SIDE FORCE FORMULA

A

F

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9
Q

ROLLING MOMENT FORMULA

A

(C-D) x b/2

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10
Q

YAWING MOMENT FORMULA

A

(A-B) x b/2

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11
Q

PITCHING MOMENT FORMULA

A

E x c

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12
Q

OTHER TYPES OF COMPONENT BALANCE

A

three component balance, two component balance

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13
Q

an incredibly complicated device, much better left to engineers of balancing than to engineers of tunnels

A

wind tunnel balance

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14
Q

placed outside the model, inside or outside the wind tunnel test section, always introduce some interference in the wind flow

A

external force balance

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15
Q

placed inside the model, no interferences, mechanical support is always needed

A

internal force balance

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16
Q

model mount of external balance

A

two strut, three strut

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17
Q

model mount for internal or external balance

A

single strut, sting

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18
Q

compromise between the required maximum load capability of all components and the accuracy required for minimum loads

A

wind tunnel balance

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19
Q

danger in inner balance

A

model can unintentionally exceed the ability of the balance

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20
Q

important to use a thorough analysis

A

external balance

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21
Q

has to bear are primarily a feature of the size and speed of the tunnel test section

A

estimated loads

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22
Q

if a tunnel size is doubled

A

platform and loads are increased fourfold

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23
Q

four external balances

A

wire, frame, yokes and pyramid

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24
Q

usually mounted inverted

A

wire balances

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25
why are wire balances mounted inverted
so the aerodynamic lift applied to the weight prevents the wires from being removed
26
much less stable and flexible, used since in the early days of aeronautics, consumes a large area
wire balances
27
these balances provide mechanisms for changing the AOA and yaw and transmit the model loads down into a system linkages
platform, yoke, and pyramid balances
28
minimizes deflection in linkage type
rigid strut
29
interaction loads can be reduce to a small value
choosing proper linkages
30
can be encountered in high speed flows
deflections
31
___ is more when three point strut support is exhibited
interference drag
32
one of the most troublesome problems of wind tunnel balances
lack of rigidity
33
____ may move the model from the resolving center and invalidate the moment data or nullify the balance alignment
deflections in the balance
34
must be kept down to where they are negligible or they must be evaluated and accounted for in the data reduction process
deflection
35
greatest source of deflection
mounting mechanism
36
solution to mounting mechanism
use high-modulus elasticity materials for the strut, have a deep and stable structure
37
large number of ____ are the main components of an external balance and are built to have minimal deflection under high load.
levers
38
knife edges
early pivots in wind tunnel balances
39
benefits of flexures
may be designed to withstand loads between the couples members in either direction with no loss of motion, practically frictionless and thus reduce symptoms of hysteresis, can survive treatment which is relatively harsh, practically wearproof; remain constant for an infinite period of time
40
wind tunnel measurements (pressure)
manometer, barometer, pressure transduces
41
balanced by the weight of the liquid column
manometer
42
used to measure atmospheric pressure
barometer
43
converts pressure to an analog electrical signal
pressure transduces
44
why do we calibrate
ensure accuracy, control error, help assure precise measurement
45
properties measured during calibration
air speed, floor angularity, turbulence measurement
46
determines airspeed inside test section
pitot tube
47
done when there is no model inside test section
setting the speed
48
usually determined by measuring either static or total pressure
tunnel speed
49
subscript for bellmouth or settling chamber
L
50
subscript for the region before testing section
S
51
usually measured throughout selected regions of the test section with the use of pitot-static tube
dynamic pressure
52
calculated from a barometric pressure measurement, and a test-section temperature determination along w/ the equation of state
density
53
variation of q in the working range of the jet
less than 0.5% from the mean, corresponds to a 0.25% variation in velocity
54
has to be uniform across the cross section
flow
55
can be calculated using sphere type and claw type yaw meter
flow direction
56
desirable variation
less than +-0.10 degrees
57
maximum variation
+-0.20 degrees
58
measurement of irregularity in the flow
turbulence
59
used to identify whether the flow is laminar or turbulent
reynolds number
60
previously used as the primary way to measure relative turbulence of a wind tunnel
turbulence sphere
61
common way to measure relative turbulence of a wind tunnel
hot-wire anemometry
62
can be measured using rakes of pitot tube
tunnel boundary layers
63