HYERSONIC AIR-BREATHING ENGINE INLET ANALYSIS

Award Information

Agency: Department of Defense	Branch: Navy	Award ID: 110	Program Year/Program: 1983 / SBIR
Agency Tracking Number: 110	Solicitation Year: N/A	Solicitation Topic Code: N/A	Solicitation Number: N/A

Small Business Information: Computational Mechan
7800 Shoal Creek Austin, TX 78757 0102
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Woman-Owned: No

Minority-Owned: No

HUBZone-Owned: No

Phase 1: Fiscal Year: 1983

Title: HYERSONIC AIR-BREATHING ENGINE INLET ANALYSIS

Agency / Branch: DOD / NAVY

Contract: N/A

Award Amount: $49,859.00

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

Principal Investigator:

Business Contact:
Dr. A.j. Baker
6155771982

Small Business Information at Submission:

Computational Mechanics
3601a Chapman Highway Knoxville, TN 37920

EIN/Tax ID:

DUNS: N/A

Number of Employees:

Woman-Owned: No

Minority-Owned: No

HUBZone-Owned: No