Considerations in the Selection of Inflow States with Finite-State Dynamic Inflow
暂无分享,去创建一个
[1] David A. Peters,et al. Theoretical prediction of dynamic inflow derivatives , 1980 .
[3] Chengjian He,et al. Validation of the FLIGHTLAB virtual engineering toolset , 2018, The Aeronautical Journal.
[4] D. Peters,et al. Correlation of Measured Induced Velocities with a Finite-State Wake Model , 1991 .
[5] W. Kinner,et al. Die kreisförmige Tragfläche auf potentialtheoretischer Grundlage , 1937 .
[6] David A. Peters. How Dynamic Inflow Survives in the Competitive World of Rotorcraft Aerodynamics , 2009 .
[7] Aviv Rosen,et al. New Actuator-Disk Model for a Skewed Flow , 2013 .
[8] David A. Peters,et al. Finite-State Induced-Flow Model for Rotors in Hover and Forward Flight , 1989 .
[9] Ohad Gur,et al. Novel Approach to Axisymmetric Actuator Disk Modeling , 2008 .
[10] Zhongyang Fei,et al. Fundamental Solutions of the Potential Flow Equations for Rotorcraft with Applications , 2015 .
[11] David A. Peters,et al. Finite state induced flow models. II - Three-dimensional rotor disk , 1995 .