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Altitude Effects - Fluid Flow Transition and Continuum Breakdown

Award Information

Agency:
Department of Defense
Branch:
Army
Award ID:
63074
Program Year/Program:
2003 / SBIR
Agency Tracking Number:
A022-1262
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
Combustion Research and Flow Technology, Inc.
6210 Kellers Church Road Pipersville, PA -
View profile »
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 1
Fiscal Year: 2003
Title: Altitude Effects - Fluid Flow Transition and Continuum Breakdown
Agency / Branch: DOD / ARMY
Contract: DAAH01-03-C-R13
Award Amount: $119,975.00
 

Abstract:

The innovation entails the extension of newly developed hypersonic transitional models and hybrid continuum/DSMC methodology to analyze plume and divert jet interactions at altitudes above 45km where present predictive capabilities are deficient due tocomplexities in the physics. In the altitude regime of 45-60 km, the separation zone generated by the interaction of the plume or divert jet with the missile aerodynamic flow is very large and laminar to turbulent transition occurs within this zone.Extensions of 3D PDE?s for kL (laminar fluctuations) and for G (intermittency), now used in the CRAFT CFD Navier-Stokes code for transitional hypersonic aerodynamic flows, will be formulated for plume-induced separated zone transition. For altitudes above60 km, continuum breakdown occurs and we will include slip regime boundary conditions into the CRAFT CFD continuum code as well as initiate formal one-way coupling of this code with the DAC DSMC code under assumptions of thermal equilibrium at the Birdbreakdown surface. Exploratory computational studies of generic missile/plume interactive flows will be performed encompassing the 45-80 km altitude regime with an optional task addressing non-continuum effects for a higher altitude divert jet problem.CRAFT Tech has played a leading role in supporting systems and developmental studies related to missile plume interactive flows in the lower endo regime. Overall support to date from both DoD and industry for such studies has been significant. Thiseffort will provide for the extension of such activities to the higher endo regime and the lower exo regime, permitting us to deal with a much broader array of problems. Particular areas where we see major commercialization potential include: (1) supportof MDA/MSIC Boost Phase Intercept studies for detection, discrimination and plume to hardbody handover; (2) Liquid and Solid threat simulant booster design (for target usage) where we have been supporting a number of industrial groups; and (3) Army effortsrelated to interceptor missile technology where divert jet effects at higher altitudes are of major concern.

Principal Investigator:

John L. Papp
Research Scientist
2152499780
jpapp@craft-tech.com

Business Contact:

Sanford M. Dash
President & Chief Scienti
2152499780
dash@craft-tech.com
Small Business Information at Submission:

COMBUSTION RESEARCH & FLOW TECHNOLOGY, I
174 North Main Street, P.O. Box 1150 Dublin, PA 18917

EIN/Tax ID: 232759059
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No