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COMMERCE BUSINESS DAILY ISSUE OF JULY 18,1996 PSA#1639Naval Surface Warfare Center, Dahlgren Division, 17320 Dahlgren Road,
Dahlgren, Virginia 22448-5100 14 -- UPGRADES AND CALCULATIONS TO THE SM-2 BLK IV AND ENHANCED SEA
SPARROW MISSILE (ESSM) FLYOUTS SOL N00178-96-Q-0223 DUE 080696 POC
Roberta C. Moss, Purchasing Agent 540-653-4304. The Naval Surface
Warfare Center, Dahlgren Division, Dahlgren, VA shall use Simplified
Acquisition procedures to place an order with combustion research and
flow technology, 174 North Main Street, Bldg 3, Dublin, PA 18917 on a
sole source basis. Combustion research is the developer of the Craftech
Navier-Stokes Code. This code is the main computer code used for the
solution of computational fluid dynamics. It has the unique capability
of handling two phase flow present in solid rocket exhausts, which is
essential for the determination of thermal loads on the ablative
lining of current Navy launchers. Large codes, such as Craft, require
a large expenditure of time to develop a working knowledge of its use
and capabilities. Three dimensional computational fluid dynamics
calculations are intensive, consuming large amounts of computer time.
Queing policies in major computer centers discourage the use of
non-parallel codes. Parallelization is essential for the shortening of
solution time and the feasibility of the three dimensional CFD
calculations. While not proprietary, the Craft code is a tightly
controlled research code by the U.S. Army Missile Command (MICOM) the
principal sponsor of the code. The code has not been released for
general use and is limited to Craftech, the principal developer and a
few groups within the DOD. Although it is possible that another company
could propose alternate codes for the calculations, extensive
modifications such as adding implicit fully coupled particle equations
which have already been included in the Craft code. In addition, the
capabilities of the codes would have to be evaluated by performing
calculations such as the VLS uptake Plume Environment, before
application to the VLS canister flow could begin. The Craft code has
already met this process and has been identified as the code best
suited for missile launcher environment, which makes combustion
research unique in its capabilities as they are the developer. In
addition to the Craft code, combustion research is thoroughly familiar
with NSWCDD's Vertical Launching System, which is the system needing
the calculations to be performed on. Under the procurement, the
contractor shall perform the following: the contractor shall provide
the necessary labor and materials to calculate the transient heating
environment and pressure loading for the MK 21 canister during a
SM-2BLK IV Missile Flyout, using the Craftcode. The contractor shall
also calculate the uptake Plume and Wind induced loads on an ESSM
Missile during a VLS Flyout and to provide CG loading as a function of
height above deck, using the Craftcode. The contractor shall also
upgrade the no-slip boundary condition of Craft with compressible wall
function; validate the upgrade via comparisons with pure Craft pipe
flow solutions utilizing fully resolved boundary layers; perform an
Axisymmetric CCL Flow Field calculation to demonstrate the utility of
this approach for realistic launcer problems; develop a domain
decomposition version of the Craft code with two phase and K-E
Turbulence capabilities for IBM SP2 parallel computer; perform
efficiency studies and Benchmarks for a CCL launcher; design a
specialized version with patching; and document the Benchmarks and
modifications. As GFM under this procurement, NSWCDD shall provide a
copy of mechanical interface control document (MICD) which contains
missile dimensions and rocket motor information; other necessary rocket
motor and particular date for constructing flow input files; AFT
closure rupture pressure and effective flow area at bottom of canister;
and grid input files for the CCL launcher. As a result of this
procurement, the contractor shall provide: an estimate of the number of
Cray C90 hours to calculate the solution for the SM-2 BLK IV Flyout;
documents of results of the calculations and a report of the results;
modified source code and input and output files required for NSWCDD to
duplicate the results. Reference quote N00178-96-Q-0223. Procurement
point of contact is Roberta C. Moss, phone 540-653-4304, fax
540-653-7016. (0198) Loren Data Corp. http://www.ld.com (SYN# 0301 19960717\14-0001.SOL)
14 - Guided Missiles Index Page
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