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M. Lighthill (1953)
Oscillating Airfoils at High Mach NumberJournal of the Aeronautical Sciences, 20
H. Tijdeman, R. Seebass (1980)
Transonic Flow Past Oscillating AirfoilsAnnual Review of Fluid Mechanics, 12
K. Hall (1994)
EIGENANALYSIS OF UNSTEADY FLOW ABOUT AIRFOILS, CASCADES, AND WINGSAIAA Journal, 32
(1993)
Computational Aeroacoustics
P. Greco, C. Lan, Tae Lim (1995)
Unsteady Transonic Aerodynamics in Frequency Domain and Calculation of Flutter Characteristics of Aircraft
Michael Romanowski, E. Dowell (1996)
Reduced order Euler equations for unsteady aerodynamic flows - Numerical techniques
R. Florea, K. Hall, P. Cizmas (1998)
Reduced-Order Modeling of Unsteady Viscous Flow in a Compressor CascadeAIAA Journal, 36
M. Karpel (1980)
Design for Active Flutter Suppression and Gust Alleviation Using State-Space Aeroelastic ModelingJournal of Aircraft, 19
B. Epureanu, K. Hall, E. Dowell (2001)
Reduced-order models of unsteady viscous flows in turbomachinery using viscous-inviscid couplingJournal of Fluids and Structures, 15
K. Hall, Jeffrey Thomas, E. Dowell (1999)
Reduced-order modelling of unsteady small-disturbance flows using a frequency-domain proper orthogonal decomposition technique
D. Tang, J. Henry, E. Dowell (1999)
LIMIT CYCLE OSCILLATIONS OF DELTA WING MODELS IN LOW SUBSONIC FLOWAIAA Journal, 37
K. Hall, R. Florea, P. Lanzkron (1994)
A Reduced Order Model of Unsteady Flows in TurbomachineryJournal of Turbomachinery-transactions of The Asme, 117
D. Nixon (1989)
Unsteady transonic aerodynamics
Michael Romanowski (1996)
Reduced order unsteady aerodynamic and aeroelastic models using Karhunen-Loeve eigenmodes
R. Vepa (1976)
On the use of Pade approximants to represent unsteady aerodynamic loads for arbitrarily small motions of wings
T. Ueda, E. Dowell (1982)
Flutter Analysis Using Nonlinear Aerodynamic ForcesJournal of Aircraft, 21
H. Troger, A. Steindl (1991)
Nonlinear stability and bifurcation theory
E. Dowell, K. Hall, Jeffrey Thomas, R. Florea, B. Epureanu, J. Heeg (1999)
Reduced order models in unsteady aerodynamics, 1
R. Parker (1967)
Resonance effects in wake shedding from parallel plates: Calculation of resonant frequenciesJournal of Sound and Vibration, 5
P. Greco, C. Lan (1997)
Frequency domain unsteady transonic aerodynamics for flutter and limit cycle oscillation predictionJournal of The Brazilian Society of Mechanical Sciences and Engineering, 32
W. Silva (1993)
Application of nonlinear systems theory to transonic unsteady aerodynamic responses, 30
E. Dowell (1970)
Generalized aerodynamic forces on a flexible plate undergoing transient motion in a shear flow with an application to panel flutterAIAA Journal, 9
M. Baker, D. Mingori, P. Goggin (1996)
Approximate Subspace Iteration for constructing internally balanced reduced order models of unsteady aerodynamic systems
J. Edwards (1979)
Applications of Laplace transform methods to airfoil motion and stability calculations
E. Dowell, M. Chi (1977)
Variable Thickness Shear Layer Aerodynamics RevisitedAIAA Journal, 15
J. Miles (1967)
On the generation of surface waves by shear flows. Part 5Journal of Fluid Mechanics, 30
R. Florea, K. Hall, P. Cizmas (1996)
Reduced order modelling of unsteady viscous flow in a compressor cascade
R. Florea, K. Hall, E. Dowell (2000)
Eigenmode Analysis and Reduced-Order Modeling of Unsteady Transonic Potential Flow Around AirfoilsJournal of Aircraft, 37
B. Winther, P. Goggin, J. Dykman (1998)
Reduced order dynamic aeroelastic model development and integration with nonlinear simulation
Taehyoun Kim (1998)
Frequency-Domain Karhunen -Loeve Method and Its Application to Linear Dynamic SystemsAIAA Journal, 36
E. Dowell, K. Hall, Michael Romanowski (1997)
Eigenmode Analysis in Unsteady Aerodynamics: Reduced Order ModelsApplied Mechanics Reviews, 50
K. Tang, W. Graham, J. Peraire (1996)
Active flow control using a reduced order model and optimum control
[Modeling of aerodynamic forces has now moved beyond the classical potential flow theory at least in the research community and to some degree in engineering practice. These more sophisticated fluid models are based upon the Euler or Navier- Stokes equations and require substantial computer resources. This has led to the search for reduced order models that retain the higher physical fidelity of such flow models while still permitting computationally feasible solutions as described in this chapter.]
Published: Oct 16, 2021
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