New developments in vibration reduction with actively controlled trailing edge flaps-Reference-Cited by-同舟云学术

New developments in vibration reduction with actively controlled trailing edge flaps

Published:2001-05 Issue:10-11 Volume:33 Page:1055-1083
ISSN:0895-7177
Container-title:Mathematical and Computer Modelling
language:en
Short-container-title:Mathematical and Computer Modelling

Author:

Friedmann P.P.,de Terlizzi M.,Myrtle T.F.

Publisher

Elsevier BV

Subject

Computer Science Applications,Modeling and Simulation

Reference33 articles.

1. Helicopter vibrations, a technological perspective;Loewy;AHS Journal,1984

2. Helicopter vibration control: A survey;Reichert;Vertica,1981

3. Vibration reduction in rotorcraft using active control: A comparison of various approaches;Friedmann;Journal of Guidance, Control, and Dynamics,1995

4. Vibration reduction in hingeless rotors using an actively controlled partial span trailing edge flap located on the blade;Millott;NASA CR-4611,1994

5. Helicopter vibration reduction with trailing edge flaps, AIAA Paper 95-1227-CP;Milgram;Proceedings of the 36th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, New Orleans, LA,10121995

Cited by 39 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aerodynamic Characteristics of A Compound Deflected LEF/TEF Rotor;Lecture Notes in Electrical Engineering;2022-08-31

2. Low Reynolds number aerodynamics of leading-edge and trailing-edge hinged control surfaces: Part I statics;Aerospace Science and Technology;2020-04

3. Numerical assessment of a deformable trailing-edge flap on aerodynamic load control of a pitching S809 airfoil using OpenFOAM;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2019-04

4. The influence of oscillating trailing-edge flap on the dynamic stall control of a pitching wind turbine airfoil;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2019-03-28

5. Design optimization of helicopter rotor using kriging;Aircraft Engineering and Aerospace Technology;2018-09-03