Aeromechanical stability of rotorcraft with advanced geometry blades-Reference-Cited by-同舟云学术

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Aeromechanical stability of rotorcraft with advanced geometry blades

Published:1994-02 Issue:3-4 Volume:19 Page:159-191
ISSN:0895-7177
Container-title:Mathematical and Computer Modelling
language:en
Short-container-title:Mathematical and Computer Modelling

Author:

Bir G.S.,Chopra I.

Publisher

Elsevier BV

Subject

Computer Science Applications,Modeling and Simulation

Reference13 articles.

1. Study of unsteady transonic flow on rotor blade with different tip shapes;Desopper;Vertica,1985

2. Etudes de profils et d'extremites de pale d'helicoptere;Thibert;Paper No. 334,1982

3. Aerodynamic design of advanced rotors with new tip shapes;Philippe;39th Annual Forum of the American Helicopter Society,1983

4. Investigation of the effect of blade sweep on rotor vibratory loads;Tarzanin;NASA CR-166526,1983

Cited by 11 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. Analysis of the Influence of Structural Parameters on the Aeroelastic Stability of Rotor Blades;Lecture Notes in Electrical Engineering;2024

2. Aeromechanical Stability of a Bearingless Rotor Helicopter with Double-Swept Blades;Journal of Aircraft;2021-03

3. Several Concerns of Advanced Airships for Thrust-vectoring Application on Dynamic Study;23rd AIAA Lighter-Than-Air Systems Technology Conference;2017-06-02

4. Optimal Design and Acoustic Assessment of Low-Vibration Rotor Blades;International Journal of Rotating Machinery;2016

5. Flutter analysis of fixed and rotary wings through a one-dimensional unified formulation;Composite Structures;2015-12

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