Geometrically Exact Aeroelastic Stability Analysis of Composite Helicopter Rotor Blades in Hover by Updated VABS-Reference-Cited by-同舟云学术

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Geometrically Exact Aeroelastic Stability Analysis of Composite Helicopter Rotor Blades in Hover by Updated VABS

Published:2024-03 Issue:2 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Shang Lina¹,Xia Pinqi²

Affiliation:

1. Lecturer, College of Aerospace Engineering, National Key Laboratory of Rotorcraft Aeromechanics, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China.

2. Professor, College of Aerospace Engineering, National Key Laboratory of Rotorcraft Aeromechanics, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5259

Reference36 articles.

1. Aeroelastic Stability Analysis of Curved Composite Blades in Hover Using Fully Intrinsic Equations

2. Composite Blade Twist Modification by Using a Moving Mass and Stiffness Tailoring

3. The effect of a movable mass on the aeroelastic stability of composite hingeless rotor blades in hover

4. Lag-twist coupling sensitivity and design for a composite blade cross-section with D-spar

5. Development of Mach Scale Rotors with Tailored Composite Coupling for Vibration Reduction

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