-
1
-
-
24144479484
-
Aeroelastic calculations for the hawk aircraft using the euler equations
-
doi:10.2514/1.5608
-
Woodgate, M. A., Badcock, K. J., Rampurawala, A. M., Richards, B. E., Nardini, D., and Henshaw, M. J., "Aeroelastic Calculations for the Hawk Aircraft Using the Euler Equations," Journal of Aircraft, Vol.42, No.4, 2005, pp. 1005-1012. doi:10.2514/1.5608
-
(2005)
Journal of Aircraft
, vol.42
, Issue.4
, pp. 1005-1012
-
-
Woodgate, M.A.1
Badcock, K.J.2
Rampurawala, A.M.3
Richards, B.E.4
Nardini, D.5
Henshaw, M.J.6
-
2
-
-
1342283898
-
Reduced-order modeling: New approaches for computational physics
-
doi:10.1016/j.paerosci.2003.12.001
-
Lucia, D. J., Beran, P. S., and Silva, W. A., "Reduced-Order Modeling: New Approaches for Computational Physics," Progress in Aerospace Sciences, Vol. 40, No. 1-2, 2004, pp. 51-117. doi:10.1016/j.paerosci.2003.12.001
-
(2004)
Progress in Aerospace Sciences
, vol.40
, Issue.1-2
, pp. 51-117
-
-
Lucia, D.J.1
Beran, P.S.2
Silva, W.A.3
-
3
-
-
34147190381
-
An investigation of the sensitivity of F-16 fighter flutter onset and limit cycle oscillations to uncertainties
-
Newport, RI, May
-
Thomas, J. P., Dowell, E. H., Hall, K. C., and Denegri, C. M., "An Investigation of the Sensitivity of F-16 Fighter Flutter Onset and Limit Cycle Oscillations to Uncertainties," 47th AIAA/ASME/ASCE/AHS/ ASC Structures. Structural Dynamics and Materials Conference, AIAA Paper 2006-11847, Newport, RI, May, 2006.
-
(2006)
47th AIAA/ASME/ASCE/AHS/ ASC Structures. Structural Dynamics and Materials Conference, AIAA Paper 2006-11847
-
-
Thomas, J.P.1
Dowell, E.H.2
Hall, K.C.3
Denegri, C.M.4
-
4
-
-
0032686725
-
Hopf-bifurcation analysis of airfoil flutter at transonic speeds
-
doi:10.2514/2.2447
-
Morton, S. A., and Beran, P. S., "Hopf-Bifurcation Analysis of Airfoil Flutter at Transonic Speeds," Journal of Aircraft, Vol.36, No.2, 1999, pp. 421-429. doi:10.2514/2.2447
-
(1999)
Journal of Aircraft
, vol.36
, Issue.2
, pp. 421-429
-
-
Morton, S.A.1
Beran, P.S.2
-
5
-
-
2542489301
-
The application of sparse matrix techniques for the CFD based aeroelastic bifurcation analysis of a symmetric aerofoil
-
doi:10.2514/1.9584
-
Badcock, K. J., Woodgate, M. A., and Richards, B. E., "The Application of Sparse Matrix Techniques for the CFD Based Aeroelastic Bifurcation Analysis of a Symmetric Aerofoil," AIAA Journal, Vol. 42, No.5, 2004, pp. 883-892. doi:10.2514/1.9584
-
(2004)
AIAA Journal
, vol.42
, Issue.5
, pp. 883-892
-
-
Badcock, K.J.1
Woodgate, M.A.2
Richards, B.E.3
-
6
-
-
22544455994
-
Direct aeroelastic bifurcation analysis of a symmetric wing based on the euler equations
-
doi:10.2514/1.5323
-
Badcock, K. J., Woodgate, M. A., and Richards, B. E., "Direct Aeroelastic Bifurcation Analysis of a Symmetric Wing Based on the Euler Equations," Journal of Aircraft, Vol. 42, No.3, 2005, pp. 731-737. doi:10.2514/1.5323
-
(2005)
Journal of Aircraft
, vol.42
, Issue.3
, pp. 731-737
-
-
Badcock, K.J.1
Woodgate, M.A.2
Richards, B.E.3
-
7
-
-
34347252618
-
Fast prediction of transonic aeroelastic stability and limit cycles
-
DOI 10.2514/1.25604
-
Woodgate, M. A., and Badcock, K. J., "On the Fast Prediction of Transonic Aeroelastic Stability and Limit Cycles," AIAA Journal, Vol.45, No.6, 2007, pp. 1370-1381. doi:10.2514/1.25604 (Pubitemid 46997902)
-
(2007)
AIAA Journal
, vol.45
, Issue.6
, pp. 1370-1381
-
-
Woodgate, M.A.1
Badcock, K.J.2
-
8
-
-
33644936546
-
Computation of smallest eigenvalues using spectral schur complements
-
doi:10.1137/040603528
-
Bekas, K., and Saad, Y., "Computation of Smallest Eigenvalues Using Spectral Schur Complements," SIAM Journal on Scientific Computing, Vol.27, No.2, 2005, pp. 458-481. doi:10.1137/040603528
-
(2005)
SIAM Journal on Scientific Computing
, vol.27
, Issue.2
, pp. 458-481
-
-
Bekas, K.1
Saad, Y.2
-
9
-
-
0000011239
-
Variational iterative methods for nonsymmetric systems of linear equations
-
April doi:10.1137/0720023
-
Eisenstat, S. C., Elman, H. C., and Schultz, M., "Variational Iterative Methods for Nonsymmetric Systems of Linear Equations," SIAM Journal on Numerical Analysis, Vol.20, No.2, April 1983, pp. 345-357. doi:10.1137/0720023
-
(1983)
SIAM Journal on Numerical Analysis
, vol.20
, Issue.2
, pp. 345-357
-
-
Eisenstat, S.C.1
Elman, H.C.2
Schultz, M.3
-
10
-
-
46449116066
-
Wing rock limit cycle oscillation prediction based on computational fluid dynamics
-
doi:10.2514/1.32812
-
Badcock, K. J., Woodgate, M. A., Allen, M. R., and Beran, P. S., "Wing Rock Limit Cycle Oscillation Prediction Based on Computational Fluid Dynamics," Journal of Aircraft, Vol.45, No.3, 2008, pp. 954-961. doi:10.2514/1.32812
-
(2008)
Journal of Aircraft
, vol.45
, Issue.3
, pp. 954-961
-
-
Badcock, K.J.1
Woodgate, M.A.2
Allen, M.R.3
Beran, P.S.4
-
11
-
-
33749322865
-
-
Rept. UMSI2004-8, Minnesota Supercomputer Inst., Univ. of Minnesota, Minneapolis, MN
-
Saad, Y., and Sosonkina, M., "Parms : A Package for the Parallel Iterative Solution of General Large Sparse Linear Systems User's Guide," Rept. UMSI2004-8, Minnesota Supercomputer Inst., Univ. of Minnesota, Minneapolis, MN, 2004.
-
(2004)
Parms : A Package for the Parallel Iterative Solution of General Large Sparse Linear Systems User's Guide
-
-
Saad, Y.1
Sosonkina, M.2
-
12
-
-
10944233712
-
Numerical analysis of store-induced limit cycle oscillarion
-
doi:10.2514/1.404
-
Beran, P. S., Knot, N. S., Eastep, F. E., Synder, R. D., and Zweber, J. V., "Numerical Analysis of Store-Induced Limit Cycle Oscillarion," Journal of Aircraft, Vol.41, No.6, 2004, pp. 1315-1326. doi:10.2514/1.404
-
(2004)
Journal of Aircraft
, vol.41
, Issue.6
, pp. 1315-1326
-
-
Beran, P.S.1
Knot, N.S.2
Eastep, F.E.3
Synder, R.D.4
Zweber, J.V.5
-
13
-
-
28844441242
-
NAL SST arrow wing with oscillating flap
-
RTO Technical Report 26, Oct.
-
Matsushita, H., Tamayama, M., Saitoh, K., and Nakamichi, J., "NAL SST Arrow Wing with Oscillating Flap," Verification an Validation Data for Computational Unsteady Aerodynamics, RTO Technical Report 26, Oct. 2000, pp. 295-318.
-
(2000)
Verification an Validation Data for Computational Unsteady Aerodynamics
, pp. 295-318
-
-
Matsushita, H.1
Tamayama, M.2
Saitoh, K.3
Nakamichi, J.4
-
14
-
-
34548328262
-
Evaluation of a simplified grid treatment for oscillating trailing-edge control surfaces
-
DOI 10.2514/1.24623
-
Rampurawala, A. M., and Badcock. K. J., "Evaluation of a Simplified Grid Treatment for Oscillating Trailing-Edge Control Surfaces," Journal of Aircraft, Vol.44, No.4, 2007, pp. 1177-1188. doi:10.2514/1.24623 (Pubitemid 47345333)
-
(2007)
Journal of Aircraft
, vol.44
, Issue.4
, pp. 1177-1188
-
-
Rampurawala, A.M.1
Badcock, K.J.2
-
15
-
-
34548310644
-
-
Ph.D. Thesis, Univ. of Glasgow, Glasgow, Scotland, U.K.
-
Rampurawala. A. M., "Aeroelastic Analysis of Aircraft with Control Surfaces using CFD," Ph.D. Thesis, Univ. of Glasgow, Glasgow, Scotland, U.K., 2006.
-
(2006)
Aeroelastic Analysis of Aircraft with Control Surfaces using CFD
-
-
Rampurawala., A.M.1
-
16
-
-
0346093756
-
Comparison of static and dynamic fluid-structure interaction solutions in the case of a highly flexible modern transport aircraftwing
-
doi:10.1016/S1270-9638(02)00007-X
-
Girodroux-Lavigne, P., Grisval, J. P., Guillemot, S., Henshaw, M., Karlsson, A., Selmin, V., et al., "Comparison of Static and Dynamic Fluid-Structure Interaction Solutions in the Case of a Highly Flexible Modern Transport Aircraft Wing," Aerospace Science and Technology, Vol.7, 2003, pp. 121-133. doi:10.1016/S1270-9638(02)00007-X
-
(2003)
Aerospace Science and Technology
, vol.7
, pp. 121-133
-
-
Girodroux-Lavigne, P.1
Grisval, J.P.2
Guillemot, S.3
Henshaw, M.4
Karlsson, A.5
Selmin, V.6
-
17
-
-
33745636385
-
A comparison of linear and nonlinear flutter prediction methods: A summary of PUMA DARP aeroelastic results
-
Allen, C. B., Jones, D., Taylor, N. V., Badcock, K. J., Woodgate, M. A., Rampurawala, A. M., et al., "A Comparison of Linear and Nonlinear Flutter Prediction Methods: A Summary of PUMA DARP Aeroelastic Results," The Aeronautical Journal, Vol. 110, No.1107, 2006, pp. 333-343.
-
(2006)
The Aeronautical Journal
, vol.110
, Issue.1107
, pp. 333-343
-
-
Allen, C.B.1
Jones, D.2
Taylor, N.V.3
Badcock, K.J.4
Woodgate, M.A.5
Rampurawala, A.M.6
-
18
-
-
0037324837
-
Extrapolation effects on coupled computational fluid dynamics/ computational structural dynamics simulations
-
doi:10.2514/2.1946
-
Goura, G. S. L., Badcock, K. J., and Woodgate, M. A., "Extrapolation Effects on Coupled Computational Fluid Dynamics/Computational Structural Dynamics Simulations," AIAA Journal, Vol.41, No.2, 2003, pp. 312-314. doi:10.2514/2.1946
-
(2003)
AIAA Journal
, vol.41
, Issue.2
, pp. 312-314
-
-
Goura, G.S.L.1
Badcock, K.J.2
Woodgate, M.A.3
-
19
-
-
28444461565
-
-
Ph.D. Thesis, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA
-
Cattarius, J., "Numerical Wing/Store Interaction Analysis of a Parametric F-16 Wing," Ph.D. Thesis, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, 1999.
-
(1999)
Numerical Wing/Store Interaction Analysis of a Parametric F-16 Wing
-
-
Cattarius, J.1
|