This report describes a mathematical model of rotorcraft that may be used to determine characteristics of performance, stability, response, and rotor blade loads. The complexity of the equations used requires the use of a digital computer for efficient solution. This four volume report describes the computer program in detail and illustrates the method of computing rotorcraft characteristics by specific example. (Author)
A Stability and Control Prediction Method for Helicopters and Stoppable Rotor Aircraft. Volume I. Engineer'S Manual
1970
87 pages
Report
No indication
English