A comprehensive analytical model of rotorcraft aerodynamics and dynamics. Part 3: Program manual
A comprehensive analytical model of rotorcraft aerodynamics and dynamics. Part 3: Program manual
- Neue Suche nach: Johnson, W.
- Neue Suche nach: Johnson, W.
The computer program for a comprehensive analytical model of rotorcraft aerodynamics and dynamics is described. This analysis is designed to calculate rotor performance, loads, and noise; the helicopter vibration and gust response; the flight dynamics and handling qualities; and the system aeroelastic stability. The analysis is a combination of structural inertial and aerodynamic models, that is applicable to a wide range of problems and a wide class of vehicles. The analysis is intended for use in the design, testing, and evaluation of rotors and rotorcraft, and to be a basis for further development of rotary wing theories. This report documents the computer program that implements the analysis.
Dokumentinformationen
A comprehensive analytical model of rotorcraft aerodynamics and dynamics. Part 3: Program manual
Zusammenfassung eines analytischen Modells der Aerodynamik und Dynamik bei Hubschraubern. Teil 3: Programmmanual
US Government Reports ; Jun ; 1-255
1980
255 Seiten
Report
Englisch