Description of Available Facilities
A comprehensive laboratory for the experimental
study of the thermomechanical behavior of materials is located
in the Center for Mechanics of Composites at Texas A&M
University. The Laboratory is equipped for experimental
research in the areas of constitutive evaluation of Materials,
structural testing, and nondestructive evaluation including
X-ray radiography, moireinterferometry, and HIPing.
Mechanical testing : Mechanical testing can
be performed on any of several different types of load frames
and/or creep frames, in order to meet the requirements of
a particular test. The load frame types include: MTS axial,
closed loop, servo hydraulic test systems with load capacities
ranging from 20 to 100 KIP's; one Adelaide axial torsional,
closed loop, screw driven test system which can simultaneously
or independently apply axial and torsional loads up to 20
KIP's and 10,000 in lbs, respectively; one MTS high rate,
open loop, servo hydraulic test system capable of accelerating
the cross head up to 60,000 in/sec and impacting a specimen
with 24,000 in lbs of energy. All of the servo hydraulic
load frames are completely automated and have data acquisition,
reduction and control software written specifically for
tests typically associated with constitutive parameter evaluation
and damage mechanics. In addition, three axial load frames
are specifically equipped with alignment fixtures and hydraulic
collet grips in order to precisely align the load train
for ceramic specimens, as well as compression testing.
The creep frames are of the direct load or
lever arm type construction and have a load capacity of
10 KIP's. The creep frames are equipped with three zone
clamshell style furnaces, capable of reaching a maximum
temperature of 2,000°F, and compatible ATS LVDT indicating
extensometry.
For elevated temperature research, the laboratory
is appropriately equipped with furnaces, extensometry, and
temperature sensing/control devices to suit a variety of
isothermal, as well as transient temperature testing requirements.
Test temperatures ranging from room temperature to 2,800°F
can be accomplished using one of several different heating
methods. The various types include: a Research Inc. 4KW
quad elliptical quartz lamp oven; an MTS three zone resistive
heating clamshell furnace; an MTS single zone, molybdenum
disilicide, rapid resistive heating furnace; a Lepel SKW
induction heating unit; and two MTS environmental chambers.
The lab is also equipped with a variety of extensometry
for low to moderate temperatures, as well as temperatures
in excess of 2800°F. Where applicable, these include:
MTS tension/compression axial (models 632.41 and 632.59)
and diametral (model 632.60) extensometers with a 1 inch
gage capacity and ceramic and/or quartz extension rods;
an MTS biaxial extensometer (model 632.85); and an assortment
of MTS axial clip gages (models 632.11, 632.12, and 632.25)
with gage capacities of 0.5 through 1 inch. Dual setpoint
digital temperature controllers, with auto-tune PID control,
can be used in conjunction with either an optical pyrometer
or thermocouples in order to precisely meet the test temperature
requirements.
Hot Isostatic Press Facility: Located in the
Department of Aerospace Engineering is a facility for the
compaction, sintering, diffusion bonding and pressing of
metal and ceramic powders. Specifications of the major items
of equipment in this laboratory are listed below. All items
and their supporting equipment are available to this project.
Hot Isostatic Press: Asea Brown Bovari model
QIC 3. Installed June, 1990. Maximum pressure: 30,000 psi.
Maximum temperature of molebdenum furnace: 1450°C. Maximum
temperature of graphite furnace: 2000°C. Dimensions
of constant temperature zone: 10 cm diameter, 11 cm high.
HIP temperature and pressure control and monitoring is programmable
from a desktop workstation (IBM PC compatible).
Cold Press: Hydraulic unit designed and fabricated
by Dr. Pollock can be configured as a unidirectional or
quasi isostatic press. Maximum force: 1000 lb. Maximum
pressure: 25,000 psi. Uses interchangeable die bodies and
rams. Accommodates articles up to 3 cm x 3cm x 10 cm in
size, and is readily modified for larger work.
Sintering Furnaces: Four furnaces of various
capacities can be programmed with multiple set points. All
have inert atmosphere capability. Vacuum sintering is done
in the HIP.
HIP Canning Facility: Necessary items for
performing the proprietary vacuum canning process are available.
Additionally, general purpose welding (TIG, MIG and oxyacetylene)
equipment is provided.
Centorr Testorr Furnace: Front access furnace,
model C-5583/20147. Vacuum/inert gas furnace which can be
mated to any one of our four MTS load frames. Temperature
capability of this furnace is 2000°C and can reach vacuum
pressures lower than 10-6 Torr. The furnace is compatible
with argon, nitrogen and helium atmospheres.
Microstructural Analysis: In addition, the
material used in any or all of the aforementioned tests
may be evaluated microstructurally by established metallographic
techniques. The lab is equiped with a Leica MEF4M metallograph,
Image-Pro imaging software, and a color laser printer for
image analysis. A Perkin Elmer Pyris 1 Differential Scanning
Calorimeter is also utilized for measurement of transformation
temperatures and latent heat associated with phase transformations.
For microstructural clarity, a Struers automatic polisher
complements the metallograph and image analysis system,
providing detailed images that can relate microstructural
changes to observed mechanical behavior.
Computational Facilities: A number of networked
PCs are available for the center, which encompass all experimental
computers. This allows for the easy transmission of test
data and results to anywhere in the world. Videoconference
capabilities are also available to allow real-time, long
distance discussion of project status and experiments with
involved parties. Supercomputers, parallel computers, and
supporting software are also available at Texas A&M
University.
ADDITIONAL MATERIALS
Laboratory Facilities
3'x4' Wind Tunnel at Texas A&M: This is
a closed circuit wind tunnel with test section dimensions
of 3'x4'. It has a contraction ratio of 9:1 and a maximum
speed of 200 ft/sec. Within the last three years, this facility
has evolved into a state of the art high productivity testing
environment for the generation of high quality aerodynamic
data with carefully quantified uncertainty bounds. The integrated
testing environment incorporates the following flow diagnostics
tools:
1. Model mount with a miniature six component
internal balance (force resolution of 1 gram) and pitch/yaw
model positioning capabilities.
2. Meso scale (7001lm) and miniature (1.4
mm) multi hole probes (5 hole and 7 hole probes) for flowfield
velocity and pressure measurements, with a five degree of
freedom probe positioning system. The current probe design
allows for steady state measurements. Efforts have already
been initiated to extent the probe frequency response to
the order of KHz by implementing MEMS based pressure transducers
(5 or 7, respectively) right at the tip of the probes. That
will enable the measurement of unsteady and turbulent flows.
3. Three-Component, Fiber-Optic Laser-Doppler
Velocimeter (LDV) for non-intrusive velocity measurements.
4. Cinematographic Particle Image Velocimeter
(CPIV) for non-intrusive instantaneous global velocimetry
(Gilarranz et. al, 1997). The system is capable of capturing
and processing of frame-rates as high as 10,000 frames/sec
and can yield, simultaneously, volumetric flowfield velocity
measurements and solid boundary motion/deformation measurements.
This type of data is of paramount importance to the microscale
flow control proposed. Two of the system's features that
enable micro-flow-diagnostics are (a) an equivalent pixel-resolution
of each image of approximately 1000x1000 and (b) the capability
of zooming the image to a physical domain of dimensions
as low as 3mm x 3mm. The combination of features (a) and
(b) yield velocity measurements on a micron scale. The project
needs will also be supported by a full-time machinist, two
part-time computer technicians, a machine shop, an electronics
and computer-repair laboratory.
Active Materials Laboratory at Texas A&M:
The Active Materials Laboratory at Texas A&M has recently
added the ability to perform non proportional loading experiments,
thermo-mechanical tests, as well as thermal analyses. In
addition, the material used in any or all of the aforementioned
tests may be evaluated microstructurally by established
metallographic techniques. A mechanical test frame with
the ability to load in tension and torsion enables successful
2-D characterization and modeling of Shape Memory Alloys
(SMAs). To this same end, the Differential Scanning Calorimeter
allows for measurement of transformation temperatures and
latent heat associated with the phase transformation present
in SMAs. In addition, a widefield metallograph and image
analysis system, complemented by a Pentium/450 computer
including the latest graphic enhancing software (Image-Pro,
Photoshop), permits the microstructural study of SMAs or
various other materials. The metallograph and image analysis
system accompany an automatic polisher and provide detailed
images that can relate microstructural changes to observed
mechanical behavior. The laboratory is also equipped with
three servo hydraulic uniaxial load frames, which state-of-the-art
digital computer hardware and software for data acquisition
and control. For theorectical modeling of SMAs, the smart
lab includes a Digital Alpha Personal Workstation 600-AU
with ABAQUS and other FE analysis software.
Department of Aerospace Engineering
Texas A&M University
1998 1999 Materials & Mechanics Laboratory
Capabilities & Pricing Sheet
Load Frames $25.00/hour
Hourly rate starts at pump on time
· 20 kip - TAMU 02-88-U-0650206 (MTS
810 22 kip) 1988 $40,000
· 50 kip - TAMU 02-91-0-0876280 (MTS
810 55 kip) 1991 $65,000
· 100 kip - TAMU 02-00-0-0250050 (MTS
880 110 kip) 1983 $150,000
· 20/10 kip - TEES 08-00-0-0420032
2000 $44,000
Adelaide Testing Machines (Tension/Torsion)
Environment Chamber $10.00/hour
Hourly rate based on run time
Carbon dioxide and argon supplied in lab
· TAMU 02-00-0-0250050 l983 $30,000
Air Furnaces $10.00/hour
Hourly rate based on run time
Carbon dioxide and argon supplied in lab
Minimum run time of 10 hours billed
· 1000°C Air Furnace TAMU
02-00-0-0250050 1983 $15,000
· 1800°C Air Furnace TAMU
02-91-0-0873455 1991 $25,000
Centorr 2000°C High Vaccum Furnace $15.00/hour
Hourly rate based on run time
Minimum run time of 10 hours billed
· TEES 08-00-0-0296928 1993 $150,000
Struers Automatic Polishing Systems $20.00/hour
Hourly rate starts at power on time
Disks, pads, and chemicals supplied in lab
· TEES 08-00-0-0396518 1997 $17,000
Perkin Elmer Pyris1 Differential Scanning
Calorimeter $15.00/hour
Hourly rate starts at power on time
Pans and accessories supplied in lab
· TEES 08-00-0-0399167 1999 $26,000
Leica MEF4M Metallograph with Digital Camera
$10.00/hour
Hourly rate starts at power on time
Color printouts are supplied at an added charge
of $.50/sheet
· TEES 08-00-0-0399185 1999 $110,000
Digital Alpha Personal Workstation 600-AU
(software included) $25.00/hour
Hourly rate starts at power on time
· TEES 08-00-0-0397801 1998 $20,000
*Training time will be billed at $25.00/hour
plus the normal rate charge for the specified equipment.
Rates may be updated to account for inflation in subsequent
years.
**Technician time will be billed at $25.00/hour.