Reduced-Order Modeling of Unsteady Aerodynamics Across Multiple Mach Regimes-Reference-Cited by-同舟云学术

Reduced-Order Modeling of Unsteady Aerodynamics Across Multiple Mach Regimes

Published:2014-11 Issue:6 Volume:51 Page:1681-1704
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Skujins Torstens¹,Cesnik Carlos E. S.¹

Affiliation:

1. Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan 48109-2140

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032222

Reference33 articles.

1. Reduced-Order Modeling of Hypersonic Vehicle Unsteady Aerodynamics

2. SilvaW. “Discrete-Time Linear and Nonlinear Aerodynamic Impulse Responses for Efficient CFD Analyses,” Ph.D. Dissertation, College of William and Mary, Williamsburg, VA, Dec. 1997.

3. Identification of Nonlinear Aeroelastic Systems Based on the Volterra Theory: Progress and Opportunities

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