Navier-Stokes calculations of inboard stall delay due to rotation
Author:
Affiliation:
1. Bell Helicopter Textron, Inc., Fort Worth, Texas 76101
2. CRAY Research, Inc., Mendota Heights, Minnesota 55120
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46127
Reference25 articles.
1. Preliminary Study of Radial Flow Effects on Rotor Blades
2. Computation of subsonic and transonic flow about lifting rotor blades
3. Conservative full-potential model for unsteady transonic rotor flows
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