Computational Wind Tunnel: A Design Tool for Rotorcraft

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX08CA61P
Agency Tracking Number: 075127
Amount: $99,527.00
Phase: Phase I
Program: SBIR
Awards Year: 2008
Solicitation Year: 2007
Solicitation Topic Code: A2.10
Solicitation Number: N/A
Small Business Information
3146 Greenwood Road, Ames, IA, 50014-4504
DUNS: 877929125
HUBZone Owned: N
Woman Owned: Y
Socially and Economically Disadvantaged: N
Principal Investigator
 Angela Lestari
 Principal Investigator
 (515) 292-9646
 nappi@sukra-helitek.com
Business Contact
 R Nappinnai
Title: Business Official
Phone: (515) 292-9646
Email: nappi@sukra-helitek.com
Research Institution
N/A
Abstract
Rotorcraft engineers traditionally use the wind tunnel to evaluate and finalize designs. Insufficient correlation between wind tunnel results and flight tests, have been often attributed in part to uncertainty in blockage corrections. Estimation of rotor blockage is significantly more complex than bluff body blockage as the correction depends on operational characteristics such as rotor RPM and thrust produced. This proposal offers to develop a design tool, which can simulate a complete rotorcraft inside a wind tunnel including all the facility effects. At the heart of the innovation are: 1. An automated hybrid grid generator. 2. A robust and economical incompressible flow solver for the grid system. 3. Momentum source based rotor model that is suitable and economical for simulating multiple rotors including the drive fans of the wind tunnel. Phase I will develop the proof-of-concept and will use unstructured Cartesian grid for the model and wind tunnel. The wind tunnel will be modeled with the diffuser, test section and nozzle. In phase II, the tool will be extended to hybrid grid with viscous grid near solid surfaces and will include drive fans of the tunnel.

* Information listed above is at the time of submission. *

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