SBIR/STTR Research Award

AIRFOIL SECTIONS

Award identifier 630b73e5fcb55dd4c386efaf1ee8ac2c2ca4a50bec74995757f0ec0c3b0b1b3fAwarding agency National Aeronautics and Space Administration

Award amount

$49,000

Program and phase

SBIR · Phase I

Award year

1983

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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

THIS IS AN ANALYTICAL STUDY OF THE VISCOUS THREE DIMENSIONAL UNSTEADY FLOW FIELD OVER AIRFOIL SECTIONS. THE LONG TERM GOAL OF THE EFORT IS DEVELOPMENT OF AN ANALYSIS THAT CAN BE APPLIED TO PREDICTING THE FLOW FIELD OVER AIRFOILS IN GENERAL AND ON HELICOPTER ROTORS IN PARTICULAR. ALTHOUGH A COMPLETE ANALYSIS IS THE LONG TERM GOAL, THE PRESENT STUDY FOCUSES UPON THE FIRST PHASE WHICH CONSIDERS THE FLOW ON A PLANAR SURFACE. THE PRESENT EFFORT MODIFIES AN EXISTING VISCOUS THREE DIMENSIONAL UNSTEADY PROCEDURE IN ORDER TO TREAT A THREE DIMENSIONAL UNSTEADY TURBULENT FLOW AND HENCE DEMONSTRATE THE CAPABILITY OF THE ANALYSIS.

Technology keywords

Not reported

Agency intelligence

National Aeronautics and Space Administration

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