SBIR/STTR Research Award

Aerodynamic Characteristics of Missile Fragments Using a Digital Wind Tunnel

Award identifier a68d96f30d115600a3d11b38350676716a47c07026ff8d37ae41d7699638cbc3Awarding agency Department of Defense · Missile Defense Agency

Award amount

$99,886

Program and phase

SBIR · Phase I

Award year

2008

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Award details

Awarding agency
Department of Defense
Branch
Missile Defense Agency
Recipient company
Flow Parametrics, LLC
Proposal award date
2008-02-13
Contract end date
2009-08-13
UEI
Not reported
Solicitation number
2007.3
Topic code
MDA07-016

Research abstract

Lift and drag characteristics of arbitray, irregularly shaped fragments will be computed using a combination of Reynolds averaged Navier-Stokes (RANS) equations and the Large-Eddy Simulation (LES) method. Cartesian meshes will be generated for the shapes, and accurate lift and drag characteristics will be post-processed using the simulation data bases. Outputs will be in the form of tables that can be utilized by existing fragment trajectory software.

Technology keywords

Not reported

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Agency intelligence

Department of Defense

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