A Preliminary Design Tool for Shrouded-Fans

Award Information
Agency: Department of Defense
Branch: Army
Contract: DAAH10-03-C-0022
Agency Tracking Number: A012-0478
Amount: $728,344.00
Phase: Phase II
Program: SBIR
Awards Year: 2003
Solicitation Year: N/A
Solicitation Topic Code: N/A
Solicitation Number: N/A
Small Business Information
3146, Greenwood road, Ames, IA, 50014
DUNS: 877929125
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Angela Lestari
 Aerospace Engineer
 (515) 292-9646
 nappi@sukra-helitek.com
Business Contact
 R. Nappinnai
Title: President
Phone: (515) 292-9646
Email: nappi@sukra-helitek.com
Research Institution
N/A
Abstract
Shrouded-fans play a key role in the U.S. Army's transportation systems. A preliminary design tool capable of simulating the flow field in different flight conditions for predicting the shroud and fan performance can significantly reduce design costs. Thisproposal offers a computational tool that will lay the foundation for true transient wake calculations of a shrouded-fan in axial and non-axial flight conditions. Phase I served to establish the proof-of-concept for such a tool. The central theme of phaseII is to convert this proof-of-concept to a user-friendly design tool with the paradigm of

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

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