-
1
-
-
84964311108
-
F-16 limit cycle oscillation testing with asymmetric store
-
AIAA-1999-3142, Norfolk, Virginia
-
Dawson, K.S. and Sussingham J.C., "F-16 Limit Cycle Oscillation Testing with Asymmetric Store", AIAA-1999-3142, AIAA Applied Aerodynamics Conference, 17th, Norfolk, Virginia, 1999.
-
(1999)
AIAA Applied Aerodynamics Conference, 17th
-
-
Dawson, K.S.1
Sussingham, J.C.2
-
2
-
-
84896856632
-
Accelerated flutter testing: A possible technique to expedite flutter testing for new aircraft
-
AIAA- 2004-6822, Summit, Woodland Hills, California
-
Harris, C., "Accelerated Flutter Testing: A Possible Technique to Expedite Flutter Testing for New Aircraft", AIAA- 2004-6822, USAF Developmental Test and Evaluation Summit, Woodland Hills, California, 2004.
-
(2004)
USAF Developmental Test and Evaluation
-
-
Harris, C.1
-
4
-
-
0035793731
-
A linearized method for the frequency analysis of three- dimensional fluid/structure interaction problems in all flow regimes
-
Lesoinne, M., Sarkis, M., Hetmaniuk, U., and Farhat, C., "A Linearized Method for the Frequency Analysis of Three- Dimensional Fluid/Structure Interaction Problems in All Flow Regimes", Computer Methods in Applied Mechanics and Engineering, Vol. 190, 2001, pp. 3121-3146.
-
(2001)
Computer Methods in Applied Mechanics and Engineering
, vol.190
, pp. 3121-3146
-
-
Lesoinne, M.1
Sarkis, M.2
Hetmaniuk, U.3
Farhat, C.4
-
5
-
-
0035390399
-
A CFD based method for solving aeroelastic eigenproblems in the subsonic, transonic, and supersonic regimes
-
Lesoinne, M., and Farhat, C., "A CFD Based Method for Solving Aeroelastic Eigenproblems in the Subsonic, Transonic, and Supersonic Regimes", AIAA Journal of Aircraft, Vol. 38, 2001, pp. 628-635.
-
(2001)
AIAA Journal of Aircraft
, vol.38
, pp. 628-635
-
-
Lesoinne, M.1
Farhat, C.2
-
6
-
-
0029138959
-
Mixed explicit/implicit time integration of coupled aeroelastic problems: Three-field formulation, geometric conservation and distributed solution
-
Farhat, C., Lesoinne, M., and Maman, N., "Mixed Explicit/Implicit Time Integration of Coupled Aeroelastic Problems: Three-Field Formulation, Geometric Conservation and Distributed Solution", International Journal in Numerical Methods in Fluids, Vol. 21, 1995, pp. 807-835.
-
(1995)
International Journal in Numerical Methods in Fluids
, vol.21
, pp. 807-835
-
-
Farhat, C.1
Lesoinne, M.2
Maman, N.3
-
7
-
-
84998879868
-
Stability analysis of dynamic meshes for transient aeroelastic computations
-
AIAA 1993-3325, Orlando, Florida, July 6-9
-
Lesoinne, M. and Farhat, C., "Stability Analysis of Dynamic Meshes for Transient Aeroelastic Computations", AIAA 1993-3325, AIAA Computational Fluid Dynamics Conference, 11th, Orlando, Florida, July 6-9, 1993.
-
(1993)
AIAA Computational Fluid Dynamics Conference, 11th
-
-
Lesoinne, M.1
Farhat, C.2
-
8
-
-
0032053181
-
Load and motion transfer algorithms for fluid/structure interaction problems with non-matching discrete interfaces: Momentum and eneergy conservation, optimal discretization and application to aeroelasticity
-
Farhat, C., Lesoinne, M., and Tallec, P., "Load and Motion Transfer Algorithms for Fluid/Structure Interaction Problems with Non-matching Discrete Interfaces: Momentum and Eneergy Conservation, Optimal Discretization and Application to Aeroelasticity", Computational Methods in Applied Mechanical Engeering, Vol. 157, 1998, pp. 95-114.
-
(1998)
Computational Methods in Applied Mechanical Engeering
, vol.157
, pp. 95-114
-
-
Farhat, C.1
Lesoinne, M.2
Tallec, P.3
-
9
-
-
0034140207
-
Two efficient staggered procedures for the serial and parallel solution of three- dimensional nonlinear transient aeroelastic problems
-
Farhat, C. and Lesoinne, M., "Two Efficient Staggered Procedures for the Serial and Parallel Solution of Three- Dimensional Nonlinear Transient Aeroelastic Problems", Computer Methods in Applied Mechanics and Engineering, Vol. 182, 2000, pp. 499-516.
-
(2000)
Computer Methods in Applied Mechanics and Engineering
, vol.182
, pp. 499-516
-
-
Farhat, C.1
Lesoinne, M.2
-
10
-
-
32044458550
-
Provably second-order time-accurate loosely-coupled solution algorithms for transient nonlinear computational aeroelasticity
-
Farhat, C., van der Zee, G. and Geuzaine, P., "Provably Second-Order Time-Accurate Loosely-Coupled Solution Algorithms for Transient Nonlinear Computational Aeroelasticity", Computer Methods in Applied Mechanics and Engineering, Vol. 195, 2006, pp. 1973-2001.
-
(2006)
Computer Methods in Applied Mechanics and Engineering
, vol.195
, pp. 1973-2001
-
-
Farhat, C.1
Van Der Zee, G.2
Geuzaine, P.3
-
11
-
-
0022131039
-
An eigensystem realization algorithm for modal parameter identification and model reduction
-
Juang, J.-N. and Pappa, R. S., "An Eigensystem Realization Algorithm for Modal Parameter Identification and Model Reduction", Journal of Guidance, Control, and Dynamics, Vol. 8, 1985, pp. 620-627.
-
(1985)
Journal of Guidance, Control, and Dynamics
, vol.8
, pp. 620-627
-
-
Juang, J.-N.1
Pappa, R.S.2
-
12
-
-
0037345147
-
Aeroelastic dynamic analysis of a full F-16 configuration for various flight conditions
-
Geuzaine, P., Brown, G., Harris, C. and Farhat, C., "Aeroelastic Dynamic Analysis of a Full F-16 Configuration for Various Flight Conditions", AIAA Journal, Vol. 41, 2003, pp. 363-371.
-
(2003)
AIAA Journal
, vol.41
, pp. 363-371
-
-
Geuzaine, P.1
Brown, G.2
Harris, C.3
Farhat, C.4
-
13
-
-
0036390834
-
Application of a three-field nonlinear fluid-structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter
-
Farhat, C., Geuzaine, P. and Brown, G., "Application of a Three-Field Nonlinear Fluid-Structure Formulation to the Prediction of the Aeroelastic Parameters of an F-16 Fighter", Computers and Fluids, Vol. 32, 2003, pp. 3-29.
-
(2003)
Computers and Fluids
, vol.32
, pp. 3-29
-
-
Farhat, C.1
Geuzaine, P.2
Brown, G.3
|