Coupled Viscous Vortex Particle Method and Unstructured CFD Solver for Rotorcraft Aerodynamic Interaction Modeling

Award Information
Agency:
Department of Defense
Branch
Navy
Amount:
$70,000.00
Award Year:
2009
Program:
STTR
Phase:
Phase I
Contract:
N68335-09-C-0334
Agency Tracking Number:
N09A-009-0132
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
Advanced Rotorcraft Technology, Inc.
1330 Charleston Rd, Mountain View, CA, 94043
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
149732315
Principal Investigator:
Chengjian He
Vice President of Research
(650) 968-1464
he@flightlab.com
Business Contact:
Donna Carrig
Vice President of Finance
(650) 968-1464
donna@flightlab.com
Research Institution:
Rensselaer Polytechnic Institute
Angela Stark
110 8th Street
Troy, NY, 12180
(518) 276-6282
Nonprofit college or university
Abstract
The helicopter rotor wake is a complicated problem and remains an extremely challenging aspect of rotorcraft performance and dynamic response analysis. The rotor/fuselage and/or rotor/ship aerodynamic interaction further complicates the problem. This STTR is dedicated to developing a solution for the complicated rotorcraft aerodynamic interaction problem. The development will couple the state-of-the-art vortex particle method (VPM) with an unstructured Navier-Stokes CFD body surface solver for a high fidelity rotor/body aerodynamic interaction simulation. The Phase I research will accomplish the formulation of the VPM/CFD coupling, prototype the coupling algorithm, and demonstrate the feasibility with rotorcraft aerodynamic interaction examples.

* information listed above is at the time of submission.

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