SBIR/STTR Research Award

PROPOSAL TO DEVELOP A NUMERICAL SIMULATION FOR THE INLET BUZZ PROBLEM BY SOLUTION OF THE TIME DEPENDENT NAVIER-STOKESEQUATIONS

Award identifier b7cd8292769fc3f10a96d39acf4a3ed348524c22ecef63b7ad7201bd1ca3502eAwarding agency National Aeronautics and Space Administration

Award amount

$205,000

Program and phase

SBIR · Phase II

Award year

1987

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
SCIENTIFIC RESEARCH ASSOC., INC.
Proposal award date
Not reported
Contract end date
Not reported
UEI
Not reported
Solicitation number
Not reported
Topic code
Not reported

Research abstract

THE PROPOSED EFFORT WOULD DEVELOP AN APPROACH FOR THE SIMULATION OF THE EXTERNAL COMPRESSION INLET FLOW FIELD VIA THE THREE-DIMENSIONAL, TIME-DEPENDENT NAVIER-STOKES EQUATIONS. WITH THIS INNOVATIVE APPROACH TO THE PROBLEM THEENTIRE FLOW FIELD WOULD BE SIMULATED VIA A SINGLE SET OF GOVERNING EQUATIONS WHICH WOULD INCLUDE DETAILS OF THE WALL VISCOUS REGION AND INCLUDE BOTH STEADY STATE AND TIME DEPENDENT SHOCK SAVE - BOUNDARY LAYER INTERACTIONS. INCLUSION OF A TIME-DEPENDENT CAPABILITY ALLOWS APPLICATION TO THE INLET BUZZ PROBLEM. THE PROPOSED APPROACH AVOIDS USING DIFFERENT APPROXIMATE EQUATIONS IN DIFFERENT PORTIONS OF THE FLOW FIELD WHICH ARE THEN JOINED THROUGH A SET OF MATCHING CONDITIONS. THEREFORE, THE PROPOSED NAVIER-STOKES SIMULATION WOULD PROVIDE A MORE POWERFUL TOOL THAN CURRENTLYEXISTS FOR THE EXTERNAL COMPRESSION INLET PROBLEM. IN ADDITION, BEING GENERAL, THIS SAME APPROACH COULD BE USED FOR BOTH MIXED AND INTERNAL COMPRESSION INLETS. UNDER PHASEI A GENERAL THREE-DIMENSIONAL CODE WOULD BE MADE APPLICABLE TO THIS PROBLEM AND A DEMONSTRATION TWO-DIMENSIONAL CALCULATION WOULD BE RUN. ASSESSMENT OF THE PROCEDURE'S CAPABILITY WOULD BE MADE VIA A COMPARISION WITH EXISTING DATA.

Technology keywords

Not reported

Agency intelligence

National Aeronautics and Space Administration

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