-
1
-
-
48749145864
-
Upwind schemes and boundary conditions with applications to Euler equations in general geometries
-
OSHER, S. and CHARKRAVARTHY, S. Upwind schemes and boundary conditions with applications to Euler equations in general geometries, J Computational Physics, 1981, 50, pp 447-481.
-
(1981)
J Computational Physics
, vol.50
, pp. 447-481
-
-
Osher, S.1
Charkravarthy, S.2
-
2
-
-
34249988639
-
Towards the ultimate conservative difference scheme II: Monotonicity and conservation combined in a second order scheme
-
VAN LEER, B. Towards the ultimate conservative difference scheme II: Monotonicity and conservation combined in a second order scheme, J Computational Physics, 1974, 14, pp 361-374.
-
(1974)
J Computational Physics
, vol.14
, pp. 361-374
-
-
Van Leer, B.1
-
3
-
-
0002374896
-
Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings
-
JAMESON, A. Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings, AIAA Paper 91-1596.
-
AIAA Paper
, vol.91
, Issue.1596
-
-
Jameson, A.1
-
4
-
-
0001097696
-
Numerical solutions of the euler equations by finite volume methods using Runge-Kutta time stepping schemes
-
SCHMIDT, W., JAMESON, A. and TURKEL, E. Numerical solutions of the euler equations by finite volume methods using Runge-Kutta time stepping schemes, 1981, AIAA-Paper 81-1259.
-
(1981)
AIAA-Paper
, vol.81
, Issue.1259
-
-
Schmidt, W.1
Jameson, A.2
Turkel, E.3
-
5
-
-
0028526832
-
A dual-time method for the solution of the unsteady euler equations
-
October
-
GAITONDE, A.L. A dual-time method for the solution of the unsteady euler equations, Aeronaut J, October 1994, 98, 978, pp 283-291.
-
(1994)
Aeronaut J
, vol.98
, Issue.978
, pp. 283-291
-
-
Gaitonde, A.L.1
-
6
-
-
0001871024
-
Time-accurate Navier-Stokes calculations with multigrid acceleration
-
NASA
-
MELSON, N.D., SANETRIK, M.D. and ATKINS, H.L. Time-accurate Navier-Stokes calculations with multigrid acceleration, 1993, Technical Report CP 3224, NASA.
-
(1993)
Technical Report
, vol.CP 3224
-
-
Melson, N.D.1
Sanetrik, M.D.2
Atkins, H.L.3
-
7
-
-
0004180896
-
-
John Wiley and Sons, Chichester, UK
-
GERADIN, M. and RIXEN, D. Mechanical Vibrations, Second edition, 1997, John Wiley and Sons, Chichester, UK.
-
(1997)
Mechanical Vibrations, Second Edition
-
-
Geradin, M.1
Rixen, D.2
-
8
-
-
0003435286
-
-
Prentice Hall, Englewood Cliffs, NJ, USA
-
BATHE, K.J. Finite Element Procedures in Engineering Analysis, 1982, Prentice Hall, Englewood Cliffs, NJ, USA.
-
(1982)
Finite Element Procedures in Engineering Analysis
-
-
Bathe, K.J.1
-
10
-
-
6344245115
-
Force transfer in aeroelastic calculations
-
December University of Bristol
-
JONES, D.P. Force transfer in aeroelastic calculations, December 2002, Technical Report AE047, University of Bristol.
-
(2002)
Technical Report
, vol.AE047
-
-
Jones, D.P.1
-
11
-
-
84985315986
-
Construction of curvilinear co-ordinates systems and applications to mesh generation
-
GORDON, W.J. and HALL, C.A. Construction of curvilinear co-ordinates systems and applications to mesh generation, Int J for Numerical Methods in Engineering, 1973, 7, pp 461 -477.
-
(1973)
Int J for Numerical Methods in Engineering
, vol.7
, pp. 461-477
-
-
Gordon, W.J.1
Hall, C.A.2
-
12
-
-
85007685430
-
A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows
-
ALBANO, E. and RODDEN, W.P. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows, AIAA J, 1969, 7, pp 179-285.
-
(1969)
AIAA J
, vol.7
, pp. 179-285
-
-
Albano, E.1
Rodden, W.P.2
-
13
-
-
0003814628
-
Subsonic unsteady aerodynamics for general configurations; Part I, Vol i - Direct application of the nonplanar doublet-lattice method
-
Airforce Flight Dynamics Laboratory
-
GIESING, J.P., KALMAN, T.P. and RODDEN, W.P. Subsonic unsteady aerodynamics for general configurations; Part I, Vol I - direct application of the nonplanar doublet-lattice method, 1971, Technical Report AFFDL-TR-71-5, Part I, Vol I, Airforce Flight Dynamics Laboratory.
-
(1971)
Technical Report
, vol.1 AFFDL-TR-71-5
, Issue.1 PART
-
-
Giesing, J.P.1
Kalman, T.P.2
Rodden, W.P.3
-
14
-
-
0015255754
-
Refinements of the nonplanar aspects of the subsonic double-lattice lifting surface method
-
RODDEN, W.P., GIESING, J.P. and KALMAN, T.P. Refinements of the nonplanar aspects of the subsonic double-lattice lifting surface method, J Aircr, 1972, 9, pp 69-73.
-
(1972)
J Aircr
, vol.9
, pp. 69-73
-
-
Rodden, W.P.1
Giesing, J.P.2
Kalman, T.P.3
-
15
-
-
0023866130
-
An efficient method for computing unsteady transonic aerodynamics of swept wings with control surfaces
-
LIU, D.D. KAO, Y.F. and FUNG, K.Y. An efficient method for computing unsteady transonic aerodynamics of swept wings with control surfaces, J Aircraft, 1988, 52, (1), pp 25-31.
-
(1988)
J Aircraft
, vol.52
, Issue.1
, pp. 25-31
-
-
Liu, D.D.1
Kao, Y.F.2
Fung, K.Y.3
-
16
-
-
0013393683
-
Standard aeroelastic configurations for "dynamic response i - Wing 445.6
-
September AGARD. Includes Tech Report TN-D-1616 as an Appendix
-
YATES, E.C. Standard aeroelastic configurations for "dynamic response I - wing 445.6, September 1985, Technical Report 765, AGARD. Includes Tech Report TN-D-1616 as an Appendix.
-
(1985)
Technical Report
, vol.765
-
-
Yates, E.C.1
-
18
-
-
0345786873
-
Prediction of transonic flutter using Nastran with aerodynamic coefficients tuned to Navier Stokes computations
-
June 1999, Norfolk,VA, USA
-
DA SILVA, R.G.A and DE FARIA MELLO, O.A. Prediction of transonic flutter using Nastran with aerodynamic coefficients tuned to Navier Stokes computations, 1999, CEAS/AIAA/ICASE/NASA meeting on Aeroelasticity and Structural Dynamics, June 1999, Norfolk,VA, USA.
-
(1999)
CEAS/AIAA/ICASE/NASA Meeting on Aeroelasticity and Structural Dynamics
-
-
Da Silva, R.G.A.1
De Faria Mello, O.A.2
-
19
-
-
38249031942
-
Recent advances in transonic computational aeroelasticity
-
BATINA, J.T., BENNETT, R.M., SEIDEL, D.A., CUNNINOHAM, H.J. and BLAND, S. Recent advances in transonic computational aeroelasticity, Computers and Fluids, 1998, 30, (172), pp 29-37.
-
(1998)
Computers and Fluids
, vol.30
, Issue.172
, pp. 29-37
-
-
Batina, J.T.1
Bennett, R.M.2
Seidel, D.A.3
Cunninoham, H.J.4
Bland, S.5
-
20
-
-
0005906008
-
Calculated viscous and scale effects on transonic aeroelasticity
-
Aalborg, Denmark, Published in AGARD R-822, October 1997.
-
EDWARDS, J.T. Calculated viscous and scale effects on transonic aeroelasticity, 1997, AGARD SMP meeting on Numerical Unsteady Aerodynamic and Aeroelastic Simulation, Aalborg, Denmark, Published in AGARD R-822, October 1997.
-
(1997)
AGARD SMP Meeting on Numerical Unsteady Aerodynamic and Aeroelastic Simulation
-
-
Edwards, J.T.1
-
21
-
-
0030245214
-
Development of a finite element aeroelastic analysis capability
-
GUPTA, K.K. Development of a finite element aeroelastic analysis capability, J Aircr, 1996, 33, (5), pp 995-1002.
-
(1996)
J Aircr
, vol.33
, Issue.5
, pp. 995-1002
-
-
Gupta, K.K.1
-
22
-
-
84982319014
-
Implementation of fully-implioit aeroelastic Navier-Stokes solver
-
29 June-2 July 1997, Snowmass Village, CO, USA, AIAA paper 97-2039, 1997
-
MELVILLE, R.B., MORTON, S.A and RIZZETTA, D.P. Implementation of fully-implioit aeroelastic Navier-Stokes solver, 1997, 13th Computational Fluid Dynamics Conference, 29 June-2 July 1997, Snowmass Village, CO, USA, AIAA paper 97-2039, 1997.
-
(1997)
13th Computational Fluid Dynamics Conference
-
-
Melville, R.B.1
Morton, S.A.2
Rizzetta, D.P.3
-
23
-
-
0027658687
-
Three-dimensional time-marching aeroelastic analyses using an unstructured-grid Euler method
-
RAUSCH, R. D., BATINA, J.T, and YANG, H.T. Three-dimensional time-marching aeroelastic analyses using an unstructured-grid Euler method. AIAA J, 1993, 31, (9), pp 1626-1633.
-
(1993)
AIAA J
, vol.31
, Issue.9
, pp. 1626-1633
-
-
Rausch, R.D.1
Batina, J.T.2
Yang, H.T.3
-
24
-
-
0001249695
-
High order subiteration-free staggered algorithm for nonlinear transient aeroelastic problems
-
LESONNE, M. and FARHAT, C. High order subiteration-free staggered algorithm for nonlinear transient aeroelastic problems. AIAA J, 1998, 36, (9), pp 1754-1757.
-
(1998)
AIAA J
, vol.36
, Issue.9
, pp. 1754-1757
-
-
Lesonne, M.1
Farhat, C.2
-
25
-
-
0034273874
-
Transonic flutter simulations using an implicit aeroelastic solver
-
GORDNIER, R.E. and MELVILLE, R.B. Transonic flutter simulations using an implicit aeroelastic solver, J Aircr, 2000, 37, (5), pp 872-879.
-
(2000)
J Aircr
, vol.37
, Issue.5
, pp. 872-879
-
-
Gordnier, R.E.1
Melville, R.B.2
-
26
-
-
33745661153
-
Evaluation of the influence of aerodynamic modelling on the transonic aeroelastic prediction of three wing test cases
-
October PUMA DARP
-
TAYLOR, N.V., JONES, D.P., GAITONDE, A., ALLEN, C.B., BADCOCK, K.J., WOODGATE, M.A., RAMPURAWAL, A.M., COOPER, J.E. and VIO, G.A. Evaluation of the influence of aerodynamic modelling on the transonic aeroelastic prediction of three wing test cases, October 2004, Technical report, PUMA DARP.
-
(2004)
Technical Report
-
-
Taylor, N.V.1
Jones, D.P.2
Gaitonde, A.3
Allen, C.B.4
Badcock, K.J.5
Woodgate, M.A.6
Rampurawal, A.M.7
Cooper, J.E.8
Vio, G.A.9
-
27
-
-
0346093756
-
Comparison of static and dynamic fluid-structure interaction solutions in the case of a highly flexible modern transport aircraft win
-
GIRODOUX-LAVIGNE, P., GRISVAL, J.P., GUILLEMOT, S., HENSHAW, M., KARLSSON, A., SELMIN, V., SMITH, J., TEUPOOTAHITI, E. and WINZELL, B. Comparison of static and dynamic fluid-structure interaction solutions in the case of a highly flexible modern transport aircraft win, J Aero Sci and Tech, 2003, 7, pp 121-133.
-
(2003)
J Aero Sci and Tech
, vol.7
, pp. 121-133
-
-
Girodoux-Lavigne, P.1
Grisval, J.P.2
Guillemot, S.3
Henshaw, M.4
Karlsson, A.5
Selmin, V.6
Smith, J.7
Teupootahiti, E.8
Winzell, B.9
-
28
-
-
85039325890
-
Comparative study of advanced fluid-structure interaction methods in'the case of a highly flexible wing
-
June 2001, Madrid
-
GIRODOUX-LAVIGNE, P., GRISVAL, J.P., GUILLEMOT, S., HENSHAW, M., KARLSSON, A., SELMIN, V., SMITH, J., TEUPOOTAHITI, E. and WINZELL, B. Comparative study of advanced fluid-structure interaction methods in'the case of a highly flexible wing, 2001, Results from the UNSI program, International Forum Aeroelasticity Structural Dynamics, June 2001, Madrid.
-
(2001)
Results from the UNSI Program, International Forum Aeroelasticity Structural Dynamics
-
-
Girodoux-Lavigne, P.1
Grisval, J.P.2
Guillemot, S.3
Henshaw, M.4
Karlsson, A.5
Selmin, V.6
Smith, J.7
Teupootahiti, E.8
Winzell, B.9
-
29
-
-
85039328987
-
-
HAASE, W., SELMIN, V. and WINZELL, B. (EDS). Vol 81 of Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Springer-Verlag
-
HAASE, W., SELMIN, V. and WINZELL, B. (EDS). Progress in Computational Flow-Structure Interaction, 2003, Vol 81 of Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Springer-Verlag.
-
(2003)
Progress in Computational Flow-structure Interaction
-
-
|