Evaluation of Finite-State Dynamic Inflow for Rotors
Author:
Affiliation:
1. U.S. Army Combat Capabilities Development Command Aviation and Missile Center Ames Research Center, Moffett Field, CA 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036208
Reference39 articles.
1. Finite‐State Induced‐Flow Model for Rotors in Hover and Forward Flight
2. Correlation of Measured Induced Velocities with a Finite‐State Wake Model
3. Finite state induced flow models. II - Three-dimensional rotor disk
4. Die kreisförmige Tragfläche auf potentialtheoretischer Grundlage
5. Influence of unsteady aerodynamics on hingeless rotor ground resonance
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1. Transient and Quasi-steady Numerical Simulations of Tiltrotor Conversion Maneuvers;J AM HELICOPTER SOC;2023
2. Transient and Quasi-steady Numerical Simulations of Tiltrotor Conversion Maneuvers;Journal of the American Helicopter Society;2023-04-01
3. Considerations in the Selection of Inflow States with Finite-State Dynamic Inflow;AIAA Journal;2021-07
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