The synopsis for this grant opportunity is detailed below, following
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document that have been posted as of
01/09/2013
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Description of Modification
Correction to Funding Opportunity Description
Document Type:
Modification to Previous
Grants Notice
Funding Opportunity Number:
BAA-RQPKC-13-04
Opportunity Category:
Discretionary
Posted Date:
Jan 09, 2013
Creation Date:
Jan 22, 2013
Original Closing Date for Applications:
Feb 25, 2013
Current Closing Date for Applications:
Feb 25, 2013
Archive Date:
Mar 27, 2013
Funding Instrument Type:
Cooperative Agreement
Category of Funding Activity:
Science and Technology and other Research and Development
Category Explanation:
Expected Number of Awards:
1
Estimated Total Program Funding:
$2,500,000
Award Ceiling:
Award Floor:
CFDA Number(s):
12.800
--
Air Force Defense Research Sciences Program
Cost Sharing or Matching Requirement:
No
Eligible Applicants
Unrestricted (i.e., open to any type of entity above), subject to any clarification in text field entitled "Additional Information on Eligibility"
Additional Information on Eligibility:
Agency Name
Air Force -- Research Lab
Description
AFRL/RQAC has a mandate to support a wide range of computational requirements for future Air Force systems. However, the initial focus for this Collaborative Center will be on developing and integrating all of the computational tools required to perform reliable, high-fidelity, multi-disciplinary analysis of high speed flows, fine-scale unsteady flows, and computational methods. As such, the CCAS will need to perform research in the following technical areas:i. High Speed Aero-Physics (for example, thermal/chemical non-equilibrium, rarefied/continuum flow, MHD, hypersonic configurations, shock-shock and shock boundary layer interactions, scramjet flow path analysis, supersonic combustion, steady and unsteady heat transfer, conjugate heat transfer, thermal loads, flow control, etc.)ii. Fine-Scale Unsteadiness (for example, boundary layers, transition prediction, turbulence excitation/suppression, turbulence models, LES/DNS, separated flow, flow control, plasma/fluidic/mechanical actuation, secondary flow, shear layers, wake flow, acoustic/EM wave propagation, etc.)iii. Enabling CFD technologies (for example, nonlinear/nonlinear fluid-structure coupling, grid motion/adaptation, generalized overset techniques, high-order and robust algorithms, uncertainty quantification, grid/geometry sensitivities, error assessment, software V&V, computational model experimental validation, interoperable/framework computing, etc.) Technical point of contact is Charles Tyler, AFRL/RQVC, Program Engineer, (937) 904-4045, charles.tyler@wpafb.af.mil.
Link to Additional Information
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The following files represent the modifications to this synopsis
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current synopsis. Changed sections from the previous document are shown
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