This User's Manual was prepared to provide the engineer with the information required to run the coupled mode version of the Normal Modes Rotor Aeroelastic Analysis Computer Program. The manual provides a full set of instructions for running the program, including calculation of blade modes, calculations of variable induced velocity distribution and the calculation of the time history of the response for either a single blade or a complete rotor with an airframe (the latter with constant inflow)
Computer programs were developed to implement the computational scheme arising from Van Holten's asy...
Methods of using rotor vacuum whirl data to improve the ability to model helicopter rotors were deve...
A mathematical model and computer program were implemented to study the main rotor free wake geometr...
The Rotor-Fuselage Analysis is a method of calculating the aerodynamic reaction between a helicopter...
A detailed description of a computer program to calculate tilt-rotor aircraft dynamic characteristic...
A mathematical model and computer program was implemented to study the main rotor free wake geometry...
The use of a computer program for a comprehensive analytical model of rotorcraft aerodynamics and dy...
An existing computer program, used for predicting the natural frequencies and mode shapes of helicop...
A computer program developed to prepare wind tunnel generated airfoil data for input into helicopter...
A user's manual for the computer program developed for the prediction of propeller-nacelle aerodynam...
A computer program used to process the equations is presented, and a full description of equation im...
Digital computer program for evaluating aerodynamic performance of rotor in flight in proximity to r...
A method was developed which permits the fully coupled calculation of fuselage and rotor airloads fo...
The differential equations of motion for the lateral and torsional deformations of a nonlinearly twi...
An efficient state-of-the-art method was developed to determine the unteady vibratory airloads produ...
Computer programs were developed to implement the computational scheme arising from Van Holten's asy...
Methods of using rotor vacuum whirl data to improve the ability to model helicopter rotors were deve...
A mathematical model and computer program were implemented to study the main rotor free wake geometr...
The Rotor-Fuselage Analysis is a method of calculating the aerodynamic reaction between a helicopter...
A detailed description of a computer program to calculate tilt-rotor aircraft dynamic characteristic...
A mathematical model and computer program was implemented to study the main rotor free wake geometry...
The use of a computer program for a comprehensive analytical model of rotorcraft aerodynamics and dy...
An existing computer program, used for predicting the natural frequencies and mode shapes of helicop...
A computer program developed to prepare wind tunnel generated airfoil data for input into helicopter...
A user's manual for the computer program developed for the prediction of propeller-nacelle aerodynam...
A computer program used to process the equations is presented, and a full description of equation im...
Digital computer program for evaluating aerodynamic performance of rotor in flight in proximity to r...
A method was developed which permits the fully coupled calculation of fuselage and rotor airloads fo...
The differential equations of motion for the lateral and torsional deformations of a nonlinearly twi...
An efficient state-of-the-art method was developed to determine the unteady vibratory airloads produ...
Computer programs were developed to implement the computational scheme arising from Van Holten's asy...
Methods of using rotor vacuum whirl data to improve the ability to model helicopter rotors were deve...
A mathematical model and computer program were implemented to study the main rotor free wake geometr...