论文信息 - Analysis of Rotor Blade Dynamics Using Model Scale UH-60A Airloads - 字舞流文

Analysis of Rotor Blade Dynamics Using Model Scale UH-60A Airloads

Michael S. Torok | R. K. Goodman | Robert K. Goodman | M. Torok

[1] John C. Houbolt,et al. Differential equations of motion for combined flapwise bending, chordwise bending, and torsion of twisted nonuniform rotor blades , 1957 .

[2] J Scheiman,et al. A TABULATION OF HELICOPTER ROTOR-BLADE DIFFERENTIAL PRESSURES, STRESSES, AND MOTIONS AS MEASURED IN FLIGHT , 1964 .

[3] Peter F. Lorber,et al. A Comprehensive Hover Test of the Airloads and Airflow of an Extensively Instrumented Model Helicopter Rotor , 1989 .

[4] Inderjit Chopra,et al. Rotor Loads Prediction Utilizing a Coupled Aeroelastic Analysis with Refined Aerodynamic Modeling , 1991 .

[5] Michael A. Marcolini,et al. The Acoustic Results of a United Technologies Scale Model Helicopter Rotor Tested at DNW , 1990 .

[6] Gloria K. Yamauchi,et al. Correlation of SA349/2 helicopter flight-test data with a comprehensive rotorcraft model , 1988 .

[7] Anton J. Landgrebe,et al. Aerodynamic and acoustic test of a United Technologies model scale rotor at DNW , 1990 .