Computational Wind Tunnel: A Design Tool for Rotorcraft

Period of Performance: 01/01/2009 - 12/31/2009

$599K

Phase 2 SBIR

Recipient Firm

Sukra Helitek, Inc.
IA
Ames, IA 50014
Principal Investigator
Firm POC

Abstract

During initial design studies, parametric variation of vehicle geometry