Aerodynamic Results of a Pressure-Instrumented Model Rotor Test at the DNW
暂无分享,去创建一个
[1] Peter F. Lorber,et al. Airfoil dynamic stall at constant pitch rate and high Reynolds number , 1987 .
[2] J Scheiman,et al. A TABULATION OF HELICOPTER ROTOR-BLADE DIFFERENTIAL PRESSURES, STRESSES, AND MOTIONS AS MEASURED IN FLIGHT , 1964 .
[3] Timothy W. Purcell. A prediction of high-speed rotor noise , 1989 .
[4] Peter F. Lorber,et al. A Comprehensive Hover Test of the Airloads and Airflow of an Extensively Instrumented Model Helicopter Rotor , 1989 .
[5] F. X. Caradonna,et al. Experimental and Analytical Studies of a Model Helicopter Rotor in Hover , 1980 .