Development of modern comprehensive computer software for rotorcraft aeromechanical analysis

• Autorzy: Narkiewicz J.
• Konferencja: Proceedings of the Fourth Seminar on Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education/seminar(IV; 30.11-02.12.2000; Warszawa, Polska)
• Języki publikacji: EN

Abstrakty

EN

A helicopter model developed by the Helicopter Mechanics Research Group at Warsaw University of Technology is presented. The model comprises main and tail rotors, fuselage and horizontal stabiliser. The model was used for investigating an influence of various factors on helicopter and rotors motion. The sample results of calculations may be used for explanation of aeromachanical phenomena in rotorcraft.

Słowa kluczowe

EN

modern computer software; aeromechanical analysis; helicopters

PL

nowoczesne oprogramowanie komputerowe; analiza aeromechaniczna; helikoptery

• Wydawca: Institute of Aeronautics and Applied Mechanics, Warsaw University of Technology
• Czasopismo: Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics
• Rocznik: 2001
• Tom: nr 12
• Strony: 7--12
• Opis fizyczny: Bibliogr. 2 poz., rys., wykr.

Twórcy

autor

Narkiewicz J.

• Warsaw University of Technology, Warsaw, Poland