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FLOW FIELD SEPARATION APPROXIMATIONS FOR HYPERSONIC AERODYNAMICS
Award Information
Agency: Department of Defense
Branch: Air Force
Contract: N/A
Agency Tracking Number: 5906
Amount:
$59,425.00
Phase:
Phase I
Program:
SBIR
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Timeline
Solicitation Year:
N/A
Award Year:
1987
Award Start Date (Proposal Award Date):
N/A
Award End Date (Contract End Date):
N/A
Small Business Information
655 S Gravers Rd
Plymouth Meeting, PA
19462
United States
DUNS:
N/A
HUBZone Owned:
No
Woman Owned:
No
Socially and Economically Disadvantaged:
No
Principal Investigator
Name: DONALD E NESTLER
Phone: (215) 825-8288
Phone: (215) 825-8288
Business Contact
Phone: () -
Research Institution
N/A
Abstract
A STUDY IS PROPOSED TO DEVELOP MORE ACCURATE APPROXIMATE METHODS FOR PREDICTING FLOW SEPARATION PHENOMENA ON HYPERSONIC MANEUVERING AEROSPACE VEHICLES. EXPERIMENTAL DATA AND FLOW FIELD COMPUTATIONS WILL BE USED TO DERIVE IMPROVED SEMI-EMPIRICAL RELATIONS FOR INCIPIENT SEPARATION, SEPARATED REGION GEOMETRY, SURFACE PROPERTIES, AND FLOW FIELD PROFILES FROM SURFACE TO INVISCID EDGE OF THE SEPARATED REGION. THE MAJOR TYPES OF FLOW SEPARATION THAT WILL BE STUDIED INCLUDE LEESIDE, WINDWARD CONTROL SURFACES, AND SHOCK IMPINGEMENT ON ADJACENT SURFACES.
* Information listed above is at the time of submission. *
