论文信息 - RAH-66 Comanche Linear Aeroservoelastic Stability Analysis: Model Improvements and Flight Test Correlation - 字舞流文

RAH-66 Comanche Linear Aeroservoelastic Stability Analysis: Model Improvements and Flight Test Correlation

Boeing | Steven J. Ingle | Bruce D. Kothmann | B. Kothmann | S. Ingle

[1] David A. Peters,et al. Theoretical prediction of dynamic inflow derivatives , 1980 .

[2] James F. Keller,et al. DESIGN AND PILOT EVALUATION OF THE RAH-66 COMANCHE CORE AFCS , 1993 .

[3] Brahmananda Panda,et al. Aeroelastic Stability Wind Tunnel Testing with Analytical Correlation of the Comanche Bearingless Main Rotor , 1997 .

[4] Inderjit Chopra,et al. An Analytical Model for a Nonlinear Elastomeric Lag Damper and Its Effect on Aeromechanical Stability in Hover , 1994 .

[5] Rene´ Mouille. The “Fenestron,” Shrouded Tail Rotor of the SA. 341 Gazelle , 1970 .

[6] Boeing Helicopters,et al. Handling Qualities of the H76 FANTAIL Demonstrator , 1991 .

[7] Alfred Gessow,et al. Aerodynamics of the Helicopter , 1981 .

[8] J. Bendat,et al. Random Data: Analysis and Measurement Procedures , 1987 .

[9] N. D. Lappos,et al. Results of Flight Tests of the Boeing/Sikorsky FANTAIL Demonstrator , 1991 .

[10] Peretz P. Friedmann,et al. Helicopter rotor dynamics and aeroelasticity - Some key ideas and insights , 1990 .

[11] R. Ganesh Rajagopalan,et al. Detailed Aerodynamic Design of the RAH-66 FANTAIL Using CFD , 1993 .

[12] Edward C. Smith,et al. Aeroelastic Response & Stability of Helicopters with Elastomeric Lag Dampers , 1996 .

[13] Inderjit Chopra,et al. An Aeroelastic Analysis Methodology for Bearingless Main Rotor Helicopters , 1998 .