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Reliable Mode Tracking for Gradient-Based Optimization with Dynamic Stability Constraints

Journal Article · · AIAA Journal
DOI:https://doi.org/10.2514/1.j061719· OSTI ID:2422329

Not provided.

Research Organization:
Rutgers Univ., Piscataway, NJ (United States)
Sponsoring Organization:
USDOE Advanced Research Projects Agency - Energy (ARPA-E)
DOE Contract Number:
AR0001186
OSTI ID:
2422329
Journal Information:
AIAA Journal, Journal Name: AIAA Journal Journal Issue: 1 Vol. 61; ISSN 0001-1452
Publisher:
AIAA
Country of Publication:
United States
Language:
English

References (19)

An Automated Procedure for Computing Flutter Eigenvalues journal February 1974
Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration journal January 2014
Gradient-Based Optimization of Solar-Regenerative High-Altitude Long-Endurance Aircraft journal November 2020
New mode tracking methods in aeroelastic analysis journal July 1995
Optimum Shape Design Against Flutter of a Cantilevered Column with an End-Mass of Finite size Subjected to a Non-Conservative load journal September 1999
Computational Modeling of Flutter Constraint for High-Fidelity Aerostructural Optimization conference January 2019
On Tracking Aeroelastic Modes in Stability Analysis Using Left and Right Eigenvectors journal October 2019
A root locus-based flutter synthesis procedure journal December 1983
Aeroelastic Optimization with an Economical Transonic Flutter Constraint Using Navier–Stokes Aerodynamics journal July 2018
Flutter and post-flutter constraints in aircraft design optimization journal August 2019
Mode tracking issues in structural optimization journal October 1995
Systematic Control Design by Optimizing a Vector Performance Index journal September 1979
Role of Unsteady Aerodynamics During Aeroelastic Optimization journal December 2015
Damping Perturbation Method for Flutter Solution: The g-Method journal September 2000
On structural optimization with aeroelasticity constraints journal August 1994
Robust structural optimization of plate wing corresponding to bifurcation in higher mode flutter journal August 2005
Use of eigenvectors in the solution of the flutter equation journal July 1993
An adaptive approach to constraint aggregation using adjoint sensitivity analysis journal December 2006
Aeroelastic Tailoring of Transport Wings Including Transonic Flutter Constraints conference January 2015

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