-
1
-
-
0003912676
-
-
ANSYS, Release 7.1. Swanson Analysis Systems, Inc
-
ANSYS, 2002. ANSYS User Manual, Release 7.1. Swanson Analysis Systems, Inc.
-
(2002)
ANSYS User Manual
-
-
-
2
-
-
0037321462
-
Theoretical and experimental investigation of the effects of a steady angle of attack on the nonlinear flutter of a delta wing plate model
-
P. Attar E. Dowell D. Tang Theoretical and experimental investigation of the effects of a steady angle of attack on the nonlinear flutter of a delta wing plate model Journal of Fluids and Structures 17 2003 243-259
-
(2003)
Journal of Fluids and Structures
, vol.17
, pp. 243-259
-
-
Attar, P.1
Dowell, E.2
Tang, D.3
-
3
-
-
27144479885
-
Modeling the LCO of a delta wing using a high fidelity structural model
-
Attar, P., Dowell, E., White, J., 2004a. Modeling the LCO of a delta wing using a high fidelity structural model. Journal of Aircraft 42 (5), 1209-1217.
-
(2004)
Journal of Aircraft
, vol.42
, Issue.5
, pp. 1209-1217
-
-
Attar, P.1
Dowell, E.2
White, J.3
-
4
-
-
16244397732
-
Modeling the LCO of a delta wing using a high fidelity structural model
-
AIAA Paper 2004-1402
-
Attar, P., Dowell, E., White, J., 2004b. Modeling the LCO of a delta wing using a high fidelity structural model, AIAA Paper 2004-1402.
-
(2004)
-
-
Attar, P.1
Dowell, E.2
White, J.3
-
5
-
-
0035441062
-
Limit cycle oscillation prediction using artificial neural networks
-
C. Denegri M. Johnson Limit cycle oscillation prediction using artificial neural networks Journal of Guidance, Control and Dynamics 24 5 2001 887-895
-
(2001)
Journal of Guidance, Control and Dynamics
, vol.24
, Issue.5
, pp. 887-895
-
-
Denegri, C.1
Johnson, M.2
-
6
-
-
0000907424
-
Eigenmode analysis in unsteady aerodynamics: Reduced order models
-
E. Dowell Eigenmode analysis in unsteady aerodynamics: Reduced order models AIAA Journal 34 8 1996 1578-1588
-
(1996)
AIAA Journal
, vol.34
, Issue.8
, pp. 1578-1588
-
-
Dowell, E.1
-
7
-
-
0242273112
-
Compact methodology for computing limit-cycle oscillations in aeroelasticity
-
B.I. Epureanu E.H. Dowell Compact methodology for computing limit-cycle oscillations in aeroelasticity Journal of Aircraft 40 5 2003 955-963
-
(2003)
Journal of Aircraft
, vol.40
, Issue.5
, pp. 955-963
-
-
Epureanu, B.I.1
Dowell, E.H.2
-
8
-
-
0001759089
-
Reduced-order models of unsteady transonic viscous flows in turbomachinery
-
B. Epureanu E. Dowell K. Hall Reduced-order models of unsteady transonic viscous flows in turbomachinery Journal of Fluids and Structures 14 2000 1215-1234
-
(2000)
Journal of Fluids and Structures
, vol.14
, pp. 1215-1234
-
-
Epureanu, B.1
Dowell, E.2
Hall, K.3
-
9
-
-
0035527633
-
Reduced-order models of unsteady viscous flows in turbomachinery using viscous-inviscid coupling
-
B. Epureanu K. Hall E. Dowell Reduced-order models of unsteady viscous flows in turbomachinery using viscous-inviscid coupling Journal of Fluids and Structures 15 2001 255-276
-
(2001)
Journal of Fluids and Structures
, vol.15
, pp. 255-276
-
-
Epureanu, B.1
Hall, K.2
Dowell, E.3
-
10
-
-
0033705043
-
Computer-aided generation of nonlinear reduced-order dynamic macromodels - I: Non-stress-stiffened case
-
L.D. Gabbay J.E. Mehner S.D. Senturia Computer-aided generation of nonlinear reduced-order dynamic macromodels - I: Non-stress-stiffened case Journal of Microelectromechanical Systems 9 2 2000 262-269
-
(2000)
Journal of Microelectromechanical Systems
, vol.9
, Issue.2
, pp. 262-269
-
-
Gabbay, L.D.1
Mehner, J.E.2
Senturia, S.D.3
-
11
-
-
0028671372
-
Eigenanalysis of unsteady flows about airfoils, cascades and wings
-
K. Hall Eigenanalysis of unsteady flows about airfoils, cascades and wings AIAA Journal 32 12 1994 2426-2432
-
(1994)
AIAA Journal
, vol.32
, Issue.12
, pp. 2426-2432
-
-
Hall, K.1
-
12
-
-
84982319130
-
Reduced-order modeling of unsteady small-disturbance flows using a frequency-domain proper orthogonal decomposition technique
-
AIAA Paper 99-0655
-
Hall, K., Thomas, J., Dowell, E., 1999. Reduced-order modeling of unsteady small-disturbance flows using a frequency-domain proper orthogonal decomposition technique, AIAA Paper 99-0655.
-
(1999)
-
-
Hall, K.1
Thomas, J.2
Dowell, E.3
-
13
-
-
0036572063
-
Computation of unsteady nonlinear flows in cascades using a harmonic balance technique
-
K. Hall J. Thomas W. Clark Computation of unsteady nonlinear flows in cascades using a harmonic balance technique AIAA Journal 40 5 2002 879-886
-
(2002)
AIAA Journal
, vol.40
, Issue.5
, pp. 879-886
-
-
Hall, K.1
Thomas, J.2
Clark, W.3
-
15
-
-
0022131039
-
An eigensystem realization algorithm for modal parameter identification and model reduction
-
J.-N. Juang R. Pappa An eigensystem realization algorithm for modal parameter identification and model reduction Journal of Guidance, Control, and Dynamics 8 1985 620-627
-
(1985)
Journal of Guidance, Control, and Dynamics
, vol.8
, pp. 620-627
-
-
Juang, J.-N.1
Pappa, R.2
-
16
-
-
0036078980
-
A parametric study of transonic airfoil flutter and limit cycle oscillation behavior
-
AIAA Paper 2002-1211
-
Kholodar, D.B., Thomas, J.P., Dowell, E.H., Hall, K.C., 2002. A parametric study of transonic airfoil flutter and limit cycle oscillation behavior, AIAA Paper 2002-1211.
-
(2002)
-
-
Kholodar, D.B.1
Thomas, J.P.2
Dowell, E.H.3
Hall, K.C.4
-
17
-
-
16244389270
-
An efficient model reduction method for linear dynamics systems with multiple inputs
-
AIAA Paper 2004-2036
-
Kim, T., 2004. An efficient model reduction method for linear dynamics systems with multiple inputs, AIAA Paper 2004-2036.
-
(2004)
-
-
Kim, T.1
-
18
-
-
33846589329
-
Aeroelastic system development using proper orthogonal decomposition and Volterra theory
-
AIAA Paper 2003-1922
-
Lucia, D., Beran, P., Silva, W., 2003. Aeroelastic system development using proper orthogonal decomposition and Volterra theory, AIAA Paper 2003-1922.
-
(2003)
-
-
Lucia, D.1
Beran, P.2
Silva, W.3
-
19
-
-
1342283898
-
Reduced order modeling: New approaches for computational physics
-
D. Lucia P. Beran W. Silva Reduced order modeling: New approaches for computational physics Progression Aerospace Sciences 40 2004 51-117
-
(2004)
Progression Aerospace Sciences
, vol.40
, pp. 51-117
-
-
Lucia, D.1
Beran, P.2
Silva, W.3
-
20
-
-
0033692191
-
Computer-aided generation of nonlinear reduced-order dynamic macromodels - II: Stress-stiffened case
-
J.E. Mehner L.D. Gabbay S.D. Senturia Computer-aided generation of nonlinear reduced-order dynamic macromodels - II: Stress-stiffened case Journal of Microelectromechanical System 9 2 2000 270-278
-
(2000)
Journal of Microelectromechanical System
, vol.9
, Issue.2
, pp. 270-278
-
-
Mehner, J.E.1
Gabbay, L.D.2
Senturia, S.D.3
-
22
-
-
0003085086
-
Reduced order unsteady aerodynamic and aeroelastic models using Karhunen-Loève eigenmodes
-
AIAA Paper 96-3981
-
Romanowski, M., 1996. Reduced order unsteady aerodynamic and aeroelastic models using Karhunen-Loève eigenmodes, AIAA Paper 96-3981.
-
(1996)
-
-
Romanowski, M.1
-
23
-
-
0041293799
-
Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques
-
AIAA Paper 1997-3712
-
Silva, W., 1997. Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques, AIAA Paper 1997-3712.
-
(1997)
-
-
Silva, W.1
-
24
-
-
20044380438
-
Reduced order models based on linear and nonlinear aerodynamic impulse response
-
AIAA Paper 1999-1262
-
Silva, W., 1999. Reduced order models based on linear and nonlinear aerodynamic impulse response, AIAA Paper 1999-1262.
-
(1999)
-
-
Silva, W.1
-
25
-
-
0043179063
-
Development of reduced-order models for aeroelastic analysis and flutter prediction using the CFL3Dv6.0 Code
-
AIAA Paper 2002-1596
-
Silva, W., Bartels, R.E., 2002. Development of reduced-order models for aeroelastic analysis and flutter prediction using the CFL3Dv6.0 Code, AIAA Paper 2002-1596.
-
(2002)
-
-
Silva, W.1
Bartels, R.E.2
-
26
-
-
0348158391
-
Development of unsteady aerodynamic state-space models from CFD-based unsteady loads
-
AIAA Paper 2001-1213
-
Silva, W.A., Reveh, D.E., 2001. Development of unsteady aerodynamic state-space models from CFD-based unsteady loads, AIAA Paper 2001-1213.
-
(2001)
-
-
Silva, W.A.1
Reveh, D.E.2
-
27
-
-
0033100467
-
Limit cycle oscillations of a cantilevered wing in low subsonic flow
-
D. Tang E. Dowell K. Hall Limit cycle oscillations of a cantilevered wing in low subsonic flow AIAA Journal 37 3 1999 364-371
-
(1999)
AIAA Journal
, vol.37
, Issue.3
, pp. 364-371
-
-
Tang, D.1
Dowell, E.2
Hall, K.3
-
28
-
-
0035422077
-
System identification and proper orthogonal decomposition method applied to unsteady aerodynamics
-
D. Tang D. Kholodar J.-N. Juang E. Dowell System identification and proper orthogonal decomposition method applied to unsteady aerodynamics AIAA Journal 39 8 2001 1569-1576
-
(2001)
AIAA Journal
, vol.39
, Issue.8
, pp. 1569-1576
-
-
Tang, D.1
Kholodar, D.2
Juang, J.-N.3
Dowell, E.4
-
29
-
-
0036531499
-
Nonlinear inviscid aerodynamic effects on transonic divergence, flutter and limit cycle oscillations
-
J. Thomas E. Dowell K. Hall Nonlinear inviscid aerodynamic effects on transonic divergence, flutter and limit cycle oscillations AIAA Journal 40 2 2002 638-646
-
(2002)
AIAA Journal
, vol.40
, Issue.2
, pp. 638-646
-
-
Thomas, J.1
Dowell, E.2
Hall, K.3
-
30
-
-
16244404935
-
Modeling limit cycle oscillation behavior of the F-16 Fighter using a harmonic balance approach
-
AIAA Paper 2004-1696
-
Thomas, J.P., Dowell, E.H., Hall, K.C., Denegri, C.M., 2004. Modeling limit cycle oscillation behavior of the F-16 Fighter using a harmonic balance approach, AIAA Paper 2004-1696.
-
(2004)
-
-
Thomas, J.P.1
Dowell, E.H.2
Hall, K.C.3
Denegri, C.M.4
|