HYERSONIC AIR-BREATHING ENGINE INLET ANALYSIS

Award Information
Agency:
Department of Defense
Branch:
Navy
Amount:
$49,859.00
Award Year:
1983
Program:
SBIR
Phase:
Phase I
Contract:
N/A
Agency Tracking Number:
110
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
Computational Mechanics
3601a Chapman Highway, Knoxville, TN, 37920
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
N/A
Principal Investigator
 () -
Business Contact
 Dr. A.j. Baker
Phone: (615) 577-1982
Research Institution
N/A
Abstract
THIS PROPOSAL DDESCRIBES AN SBIR PROJECT TO ESTABLISH AN IMPROVED ANALYITCAL TECHNIQUE IN EXTERNAL AND \ OR INTERNALLY DUCTED FLOW PROPERTIES FOR HYPERSONIC ENGINE AIR LINLETS. THE GOAL OF THIS PHASE I PROJECT IS TO CLEARLY CATEGORIZE THE DISTINGUISHING CHARACTERISTICS OF PUBLISHED CFD ALGOORITHM CONSTRUCTIONS, WITHIN A UNIFIED THEORETICAL FRAMEWORK, FOR THE HYPERSONIC INLET AERODYNAMICS PROBLEM CLASS. THIS ANALYSIS WILL YIELD QUANTIZATION OF ALGORITHM DESIGN DISTINGUISHING FATURES, INCLUDING GEMETRIC VERSATILTY, (THE NEED FOR) ARTIFICAL DIFFUSION MECHANISMS, ACCURATE INCLUSION OF VISCOTIY EFFECTS IN A HIGH MACH AND HIGH REYNOLDS NUMBER FLOW, AND MAPPING TO A VECTOR COMPUTER ARCHITECTURE (EFFICIENCY). THE COMPLETION OF THE PHASE I PROJECT WILL IDENTIFY AND OPTIMAL ALGORITHM CONSTRUCTION, IF ONE EXISTS, FOR THE CFD INLET PROBLEM CLASS, AS BASED DISTINGUISHING CHARACTERISTICS OF PUBLISHED

* information listed above is at the time of submission.

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