AIRFOIL SECTIONS

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: N/A
Agency Tracking Number: 584
Amount: $49,000.00
Phase: Phase I
Program: SBIR
Awards Year: 1983
Solicitation Year: N/A
Solicitation Topic Code: N/A
Solicitation Number: N/A
Small Business Information
Scientific Research Assoc.
P.o. Box 498, Glastonbury, CT, 06033
DUNS: N/A
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 BERNARD C. WEINBERG
 PRINCIPAL INVESTIGATOR
 () -
Business Contact
Phone: () -
Research Institution
N/A
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.

* information listed above is at the time of submission.

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