User instructions for a graphics package for coupled rotor/airframe vibration analysis are presented. Responses to plot package messages which the user must make to activate plot package operations and options are described. Installation instructions required to set up the program on the CDC system are included. The plot package overlay structure and subroutines which have to be modified for the CDC system are also described. Operating instructions for CDC applications are included
Sufficient instructions for running the subsonic/supersonic advanced panel pilot code were developed...
Sample input and output listings obtained with the base program (SIMVIB) of the coupled rotor/airfra...
The details of the modeling process and its implementation approach are presented. A generic methodo...
The Rotor-Fuselage Analysis is a method of calculating the aerodynamic reaction between a helicopter...
User instructions for the Tektronix Graphics Package of the Automated Paneling Technique (APT) and t...
This User's Manual was prepared to provide the engineer with the information required to run the cou...
A detailed description of a computer program to calculate tilt-rotor aircraft dynamic characteristic...
Rotordynamics codes for personal computers are now becoming available. One of the most capable codes...
The use of a computer program for a comprehensive analytical model of rotorcraft aerodynamics and dy...
A computer program used to process the equations is presented, and a full description of equation im...
A method was developed which permits the fully coupled calculation of fuselage and rotor airloads fo...
A mathematical model and computer program was implemented to study the main rotor free wake geometry...
The computer program documentation for the design and analysis of supersonic configurations is prese...
Background information is presented for the helicopter rotor test facility, in preface to a more det...
Personal computers can now do many jobs that formerly required a large mainframe computer. An exampl...
Sufficient instructions for running the subsonic/supersonic advanced panel pilot code were developed...
Sample input and output listings obtained with the base program (SIMVIB) of the coupled rotor/airfra...
The details of the modeling process and its implementation approach are presented. A generic methodo...
The Rotor-Fuselage Analysis is a method of calculating the aerodynamic reaction between a helicopter...
User instructions for the Tektronix Graphics Package of the Automated Paneling Technique (APT) and t...
This User's Manual was prepared to provide the engineer with the information required to run the cou...
A detailed description of a computer program to calculate tilt-rotor aircraft dynamic characteristic...
Rotordynamics codes for personal computers are now becoming available. One of the most capable codes...
The use of a computer program for a comprehensive analytical model of rotorcraft aerodynamics and dy...
A computer program used to process the equations is presented, and a full description of equation im...
A method was developed which permits the fully coupled calculation of fuselage and rotor airloads fo...
A mathematical model and computer program was implemented to study the main rotor free wake geometry...
The computer program documentation for the design and analysis of supersonic configurations is prese...
Background information is presented for the helicopter rotor test facility, in preface to a more det...
Personal computers can now do many jobs that formerly required a large mainframe computer. An exampl...
Sufficient instructions for running the subsonic/supersonic advanced panel pilot code were developed...
Sample input and output listings obtained with the base program (SIMVIB) of the coupled rotor/airfra...
The details of the modeling process and its implementation approach are presented. A generic methodo...