This report consists of three volumes and documents the current version in the C81 family of rotorcraft flight simulation programs developed by Bell Helicopter Textron. This current version of the digital computer program is referred to as AGAJ76. The accompanying program for calculating fully-coupled rotor blade mode shapes is called DN9100. The first volume, the Engineer's Manual, presents an overview of the computer program capabilities plus discussions for the background and development of the principle mathematical models in the program. The models discussed include all those currently in the program.
Rotorcraft Flight Simulation with Coupled Rotor Aeroelastic Stability Analysis. Volume I. Engineer's Manual
1977
347 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aeronautics , Rotary wing aircraft , Flight simulation , Aerodynamic stability , Numerical analysis , Rotor blades(Rotary wings) , Aeroelasticity , Resonant frequency , Flight maneuvers , Flight paths , Flow charting , Mathematical models , Computerized simulation , Digital computers , Computer programs