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POV-Ray
3.1G- 3D Rendering:::...
We
rendered the scene "Chess2" in POV Ray 3.5. The
scene was rendered at 640x480 and AA 0.3.
POV-Ray
- 32bit Windows Environment
4000+ Results - Lower is Better
FX55 Results - Lower is Better
SPECviewperf
7.1:::...
The
SPECopcSM project group made data changes to viewsets running
under SPECviewperf 7.1 to discourage optimizations that
benefit the benchmark, but might not improve real-world
application performance. Since the SPECviewperf source and
binaries have been upgraded to support some of these changes,
no comparisons should be made between past results and current
results for viewsets running under SPECviewperf 7.1.
SPECopc
project group members recognize the importance of real-world
benchmarks. From the beginning, the group has sought benchmarks
representative of the OpenGL rendering portion of independent
software vendor (ISV) applications. Along these lines, the
project group has come up with what it calls a viewset.
A viewset is a group of individual runs of SPECviewperf
that attempt to characterize the graphics rendering portion
of an ISV's application.
Currently,
there are six standard SPECopc application viewsets:
- 3dsmax-02,
based on SPECapc for 3ds max 3.1 configured with the Open
GL driver, includes three models containing an average
of 1.5 million vertices each, and tests performance of
scenes with different levels of lighting.
- dx-08,
based on IBM's Data Explorer application, has 10 different
tests.
- drv-09,
based on Intergraph's DesignReview model review package,
has five different tests.
- light-06,
based on Discreet's Lightscape radiosity application,
has four tests.
- proe-02,
based on SPECapc for Pro/ENGINEER 2001, measures two models
in three modes - shaded, wireframe and hidden-line removal
(HLR).
- ugs-03,
based on SPECapc for Unigraphics V17, tests performance
based on an engine model containing 2.1 million vertices.
4000+
Results
FX55
Results
CliBench
SMP Mk III:::...
clibench
is a suite of benchmarks, some are self developed other
are slightly modified industry standard benchmarks to check
up your computer.
4000+
Results
FX55
Results
CASE
Labs AGARD Benchmark:::...
The
benchmark testcase is the AGARD 445.6 aeroelastic test wing.
The wing uses a NACA 65A004 airfoil section and has a panel
aspect ratio of 1.65, taper ratio of 0.66, and a quarter-chord
sweep angle of 45º. This AGARD wing was tested at the
NASA Langley Research Center in the 16-foot Transonic Dynamics
Tunnel and is a standard aeroelastic test case used for
validation of unsteady, compressible CFD codes.
The
CFD grid used to model this problem consists of 67,435 nodes
and 366,407 tetrahedral elements.....so there!
4000+
Results
FX55
Results
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