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pro vyhledávání: '"Chong-Seok Chang"'
Publikováno v:
Journal of Aircraft. 47:1240-1247
High-altitude, long-endurance (HALE) aircraft are highly flexible, requiring nonlinear aeroelastic analysis. NATASHA (Nonlinear Aeroelastic Trim and Stability of HALE Aircraft) is a computer program developed to analyze the aeroelastic behavior of HA
Autor:
Dewey H. Hodges, Chong-Seok Chang
Publikováno v:
Journal of Mechanics of Materials and Structures. 4:1257-1270
Autor:
Dewey H. Hodges, Chong-Seok Chang
Publikováno v:
Journal of Mechanics of Materials and Structures. 4:675-692
The paper presents a concise framework studying the coupled vibration of curved beams, whether the curvature is built-in or is caused by loading. The governing equations used are both geometrically-exact and fully intrinsic, with a maximum degree of
Publikováno v:
Journal of Aircraft. 45:538-545
An analysis and parametric study of the flight dynamics of highly flexible aircraft are presented. The analysis extends previous work of the authors, used to predict the atypical flight dynamic characteristics of highly flexible flying wings, to conv
Autor:
Dewey H. Hodges, Chong-Seok Chang
Publikováno v:
Journal of Aircraft. 44:2049-2059
Fundamental modeling of a flexible aircraft with a flying wing configuration, attached to a system of bungee cords, was developed in previous work of the authors. Herein this work is extended to include the capability of modeling a general configurat
Adaptive planning and tracking of trajectories for the simulation of maneuvers with multibody models
Publikováno v:
Computer Methods in Applied Mechanics and Engineering. 195:7052-7072
We study the simulation of maneuvers with multibody models. We propose a framework based on a hierarchical decomposition of the problem inspired from the work on autonomous vehicles. The result is a system that not only is capable of piloting a vehic
Autor:
Chong-Seok Chang1,2, Hodges, Dewey H.1,3
Publikováno v:
Journal of Aircraft. Nov/Dec2007, Vol. 44 Issue 6, p2049-2049. 1p.
Publikováno v:
Journal of Aircraft. Jul/Aug2010, Vol. 47 Issue 4, p1240-1240. 1p.