Formulation of a Comprehensive Aeroelastic Analysis for Tilt-Rotor Aircraft-Reference-Cited by-同舟云学术

Formulation of a Comprehensive Aeroelastic Analysis for Tilt-Rotor Aircraft

Published:1998-03 Issue:2 Volume:35 Page:280-287
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Srinivas Venkataraman¹,Chopra Inderjit¹

Affiliation:

1. University of Maryland, College Park, Maryland 20742

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.2296

Reference10 articles.

1. 2Kvaternik, R. G. “Studies in Tilt-Rotor VTOL Aircraft Aeroelasticity,” Ph.D. Dissertation,Case Western Reserve Univ., Cleveland, OH, 1973.

2. 4Nixon, M. W. “Aeroelastic Response and Stability of Tiltrotors with Elastically Coupled Composite Rotor Blades,” Ph.D. Dissertation, Dept. of Aerospace Engineering, Univ. of Maryland,College Park, MD,Dec. 1993.

3. 5Srinivas, V. “Aeroelastic Analysis of Advanced Tiltrotor Aircraft,” Ph.D. Dissertation, Dept. of Aerospace Engineering, Univ. of Maryland,College Park, MD,1995.

Cited by 4 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. Chronological bibliography;Whirl Flutter of Turboprop Aircraft Structures;2015

2. Analysis of vibrations of an innovative civil tiltrotor;Aerospace Science and Technology;2013-08

3. Prediction of Tiltrotor Vibratory Loads with Inclusion of Wing-Proprotor Aerodynamic Interaction;Journal of Aircraft;2010-01

4. Vibration of adaptive wing-rotor system for tiltrotor aircraft application;41st Structures, Structural Dynamics, and Materials Conference and Exhibit;2000-04-03