Assessment of Active Controls for Rotor Performance Enhancement
暂无分享,去创建一个
[1] Roberto Celi,et al. Optimum Two-Per-Revolution Inputs for Improved Rotor Performance , 2005 .
[2] Cynthia B. Callahan,et al. Application of a comprehensive analytical model of rotorcraft aerodynamics and dynamics (CAMRAD) to the McDonnell Douglas AH-64A helicopter , 1987 .
[3] Aeroflightdynamics Directorate,et al. AEROMECHANICS OF THE ACTIVE ELEVON ROTOR , 2005 .
[4] Ahmed A. Hassan,et al. Experimental/Numerical Evaluation of Integral Trailing Edge Flaps for Helicopter Rotor Applications , 2005 .
[5] Arnold,et al. Open Loop Flight Test Results and Closed Loop Status of the IBC System on the CH-53G Helicopter , 2003 .
[6] Matthew L. Wilbur,et al. FURTHER EXAMINATION OF THE VIBRATORY LOADS REDUCTION RESULTS FROM THE NASA/ARMY/MIT ACTIVE TWIST ROTOR TEST , 2002 .
[7] Carlos E. S. Cesnik,et al. Vibratory loads reduction testing of the NASA/Army/MIT active twist rotor , 2001 .
[8] Friedrich K. Straub,et al. Rotors with Trailing Edge Flaps: Analysis and Comparison with Experimental Data , 1998 .
[9] M. S. Chandrasekhara,et al. Compressible Dynamic Stall Control Using a Variable Droop Leading Edge Airfoil , 2004 .
[10] George A. Lesieutre,et al. Miniature trailing-edge effectors for rotorcraft performance enhancement , 2007 .
[11] Matthew L. Wilbur,et al. Aerodynamic Design Study of an Advanced Active Twist Rotor , 2003 .
[12] M. Drela. Newton solution of coupled viscous/inviscid multielement airfoil flows , 1990 .
[13] Inderjit Chopra,et al. Hover Testing of Smart Rotor with Induced-Strain Actuation of Blade Twist , 1997 .
[14] J. Kentfield,et al. The potential of Gurney flaps for improving the aerodynamic performance of helicopter rotors , 1993 .
[15] Hyeonsoo Yeo,et al. Performance Analysis of a Utility Helicopter with Standard and Advanced Rotors , 2004 .
[16] Hyeonsoo Yeo,et al. Calculation of Rotor Performance and Loads Under Stalled Conditions , 2003 .
[17] Roy Y. Myose,et al. Gurney Flap Experiments on Airfoils, Wings, and Reflection Plane Model , 1998 .