Helicopter flight envelope extending while performing manoeuvres at low flight velocities

• Autorzy: Szumański K. , Bereżański J. , Szumański A.
• 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

The paper deals with the problem of helicopter flight mechanics at low flight speeds. The purpose of performed analysis is to achieve possibility of helicopter angular position control within wide range of angular displacement. This is performed by linear and centrifugal acceleration control. Rotor thrust vector control makes those accelerations appear.

Słowa kluczowe

EN

aircrafts; helicopters; helicopters manoeuvres

PL

samoloty; helikoptery; manewry śmigłowców

• 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: 2000
• Tom: nr 10
• Strony: 203--210
• Opis fizyczny: Bibliogr. 2 poz., rys., tab., wykr.

Twórcy

autor

Szumański K.

autor

Bereżański J.

autor

Szumański A.

• Institute of Aviation, Warsaw, Poland,