Recent Improvements to a Hybrid Method for Rotors in Forward Flight
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332-0150
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.3000
Reference37 articles.
1. Solution of transonic flow past rotor blades using the conservative full potential equation
2. 5Strawn, R. C., and Caradonna, F. X. “Numerical Modeling of Rotor Flows with a Conservative form of the Full Potential Equation,”AIAA Paper 86-0079, July 1986.
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