AEROLAB
STING BALANCES
Sting
Diameter & Designation |
Normal
Force |
Side
Force |
Axial
Force |
Pitching
Moment |
Yawing
Moment |
Rolling
Moment |
(INCHES) |
(LBS) |
(LBS) |
(LBS) |
(IN
LBS) |
(IN
LBS) |
(IN
LBS) |
|
|
|
|
|
|
|
EWT
Pistol |
25 |
--- |
10 |
50 |
--- |
--- |
3/8
A |
10 |
10 |
4 |
15 |
15 |
50 |
3/8
B |
15 |
10 |
6 |
22 |
15 |
50 |
3/8
C |
20 |
15 |
12 |
32 |
22 |
50 |
1/2
A |
40 |
30 |
12 |
70 |
60 |
60 |
1/2
B |
60 |
36 |
15 |
120 |
70 |
80 |
5/8
A |
100 |
75 |
25 |
200 |
156 |
150 |
5/8
B |
150 |
100 |
25 |
250 |
180 |
200 |
3/4
A |
200 |
100 |
60 |
400 |
200 |
160 |
3/4
B |
250 |
144 |
50 |
460 |
255 |
200 |
1 |
300 |
150 |
80 |
500 |
250 |
250 |
AEROLAB
has designed and built over 100 strain gauge balances for subsonic,
transonic and supersonic wind tunnels. Usually complete systems
are supplied including the model positioning linkage, power supply
and digital readout. Either manual or motorized operation is offered
for angle of attack and angle of yaw adjustment.
Internal One-Piece Balances
Internal balances are, almost universally, used for measurements
in supersonic and transonic tunnels. There are also popular in
subsonic tunnels. Recently AEROLAB has developed
an internal balanced cut from a single piece of precipitation-hardened
stainless steel. No screws, pins or welds are used. This one piece
design is superior to earlier designs in strength, accuracy and
in providing lower interactions between components. These advantages
are particularly significant in Axial Force because of its sensitivity
compared to the other components. The accompanying photograph
shows the geometry for insulating Axial Force from the other components.

Standard balances from
3/8-inch to 1-inch
Closeup of sting balance |
Referring to the
close-up, the balance is separated into halves by the diagonal
cut with the two halves joined by sixteen flexures (8 shown in
the picture and 8 on the back side). These flexures offset normal
and side loads and permit limited axial movements. The axial movement
is resisted by the cantilever beam in the center which is pulled
by the thin, flexible strip at the top. Strain gauges are installed
near the bottom of the beam to measure the strain as the beam
is deflected. The axial force measurements beam is thereby shielded
from the loads produced by normal and side forces.
Design Details
The balances are normally designed with cylindrical ends, one
of which is clamped into the model positioning system and the
other fits into a reamed hole in the model, secured with a set
screw. If desired, the balance may be fitted with a tapered end
to support the model. Two problems are commonly encountered in
the use of the internal strain gauge balances. The foil strain
gauges and the fine wires are vulnerable to rough handling; and
the sting must be enclosed in the model to protect against airflow
over the gauges (which causes erroneous readings).
Accessory Equipment
AEROLAB eliminates the problems by enclosing
the sting in a metal sheath. All balances are supplied with calibration
barrels and roll bars (for six-component models) which are individually
grooved to apply loads at known locations. Reamers are supplied
to machine models for proper fit on the balance.
Supersonic Model Positioning System
In supersonic tunnels models are generally adjusted in angle of
attack with a half quadrant, as shown in the illustration. The
model is rotated about a point near the end of the sing so it
stays substantially in the center of the test section as the angle
is varied. The quadrant is driven though a gear train by an adjusting
knob which also drives a mechanical counter indicating the angle
of attack to the nearest tenth of a degree. The quadrant is well
supported by adjustable eccentric ball bearing guides and aluminum
plates on the sides.
Supersonic tunnels are almost invariably of the blow-down type
wherein a run of short duration (typically 15 to 30 seconds) is
followed by a relatively long pump-up time (typically 3 minutes).
It is therefore advisable on the larger tunnels (4 by 4 inch and
larger) to motorize the angle of attack system and to employ a
computerized Data Acquisition System. AEROLAB
drives the angle of attack quadrant with a variable speed motor
through a Geneva Drive unit which converts the steady rotation
at input to rotation for ¼ of a cycle and stopped rotation
for ¾ of a cycle, a so-called pitch-pause drive.
The system is gear driven so that consecutive pause positions
are exactly one degree apart to ensure the accuracy of angle of
attack settings.
The smallest AEROLAB one-piece balance measures
3/8-inch in diameter, suitable for a 4 by 4 inch supersonic tunnel.
A special balance with a 3/16-inch diameter sting is offered for
the 2 by 2 inch tunnel with motorized drive option.
The AEROLAB
1 by 1 inch supersonic employs and angel of attack quadrant but
space is insufficient for a practical balance.
Subsonic Model Positioning System
Subsonic balances are usually associated with larger dimensions
and lower loads (than supersonic) which make parallelogram model
positioning system more appropriate. The parallelogram linkage
is versatile: the balance may be removed and the test section
made clean by removing the two vertical links; the
front vertical link and the balance may be removed and the rear
vertical link may be used for traversing pressure or hot wire
instruments in a vertical direction (with small stream-wise motion);
and finally additional holes can be drilled in the vertical links
for testing automobiles or models in ground effect near the floor.
Model positioning systems designed for yaw (as well as pitch)
require an opening in the floor of the test section to permit
yawing of the vertical links. For these yaw systems AEROLAB provides
an aluminum turntable. The turntable is supported by the frame
of the balance and rotates integrally with the balance in yaw.
It is only necessary for the customer to cut a circular hole in
the floor of the wind tunnel slightly larger than the turntable
diameter.
The magnitudes of angle of attack and angle of yaw are indicated
on digital counters to the nearest tenth of a degree. As an option,
the angle of attack mechanism can be driven by an adjustable speed
motor (replacing the hand adjustment) and the angle of attack
read on a digital meter with both the controls and the meter housed
in a control box. As a second option, motorized control and remote
readout of both pitch and yaw is offered.
Model positioning system with motorized angle
of attack and motorized angle of yaw.
Manual angle of yaw with mechanical counter. |
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