1 |
Fujii, K. and Schiff, L. B., 1989, 'Numerical Simulation of Vortical Flows over Strake-Delta Wing,' AIAA J., Vol. 27, pp. 1153-1162
DOI
ScienceOn
|
2 |
Grismer, D. S., 1995, 'Double-Delta-Wing Aerodynamics for Pitching Motions with and without Sideslip,' J. Aircraft, Vol. 32, pp. 1303-1311
DOI
|
3 |
Erickson, G. E., Schreiner, J. A. and Roges, L. W., 1989, 'On the Structure, Interaction, and Breakdown Characteristics of Slender Wing Vortices at Subsonic, Transonic, and Supersonic Speeds,' AIAA paper 89-3345
|
4 |
Hummel, D., 1978, 'On the Vortex Formation Over a Slender Wing at Large Angles of Incidence,' AGARD-CPP-247
|
5 |
Gortz, S., Rizzi, A. and Munukka, K., 1999, 'Computational Study of Vortex Breakdown over Swept Delta Wings,' AIAA Paper 99-3118
|
6 |
Hinze, J. O., 1975, Turbulence, McGraw-Hill Publishing Co., New York, p. 23
|
7 |
Kern, S. B., 1993, 'Vortex Flow Control Using Fillets on a Double-Delta Wing,' J. Aircraft, Vol. 30, pp. 818-825
DOI
ScienceOn
|
8 |
Kim, T. H., Kweon, Y. H., Kim, H. D. and Sohn, M. H., 2003, 'A Study of the Vortical Flow over a Delta Wing with a Leading Edge Extension,' 6th Int. Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, Shanghai, China, pp. 408-413
|
9 |
Jameson, A., Schmidt, W. and Turkel, E., 1981, 'Numerical Solution of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Schemes,' AIAA Paper 81-1259
|
10 |
Ken, C., 1993, 'Numerical Study of Blowing on Delta Wings at High Alpha,' J. Aircraft, Vol. 30, pp. 833-839
DOI
ScienceOn
|
11 |
Ekaterinaris, J. A. and Schiff, L. B., 1990, 'Numerical Simulation of the Effects of Variation of Angle of Attack and Sweep Angle on Vortex Breakdown over Delta Wings,' AIAA Paper 90-3000
|
12 |
Launder, B. E. and Spalding, D. B., 1972, Lectures in Mathematical Models of Turbulence, Academic Press, London, England
|
13 |
Lee, K. Y. and Sohn, M. H., 2003, 'The Vortical Flow Field of Delta Wing with Leading Edge Extension,' KSME Intl. J., Vol. 17, pp. 914-924
DOI
|
14 |
Lowson, M. V. and Riley, A. J., 1995, 'Vortex Breakdown Control by Delta Wing Geometry,' J. Aircraft, Vol. 32, pp. 832-838
DOI
ScienceOn
|
15 |
Robinson, B. A., Barnett, R. M. and Agrawal, S., 1994, 'Simple Numerical Criterion for Vortex Breakdown, AIAA J., Vol. 32, pp. 116-122
DOI
ScienceOn
|
16 |
Sarkar, S. and Balakrishnan, L., 1990, 'Application of a Reynolds-Stress Turbulence Model to the Compressible Shear Layer,' ICASE Report 90-18, NASA CR-182002
|
17 |
Verhaagen, N. G. and Naarding, S. H. J., 1989, 'Experimental and Numerical Investigation of the Vortex Flow over a Sidesliping Delta Wing,' J. Aircraft, Vol. 26, pp. 971-978
DOI
|
18 |
Sohn, M. H. and Lee, K. Y., 2002, 'Experimental Investigation of Vortex Flow of a Yawed Delta Wing Having Leading Edge Extension,' AIAA paper 2002-3267
|
19 |
Wentz, W. H. Jr. and Kohlman, D. L., 1971, 'Vortex Breakdown on Slender Sharp Edged Wings,' J. Aircraft, Vol. 8, pp. 156-161
DOI
|
20 |
Barth, T. J. and Jespersen, D., 1989, 'The Design and Application of Upwind Schemes on Unstructured Meshes,' AIAA Paper 89-0366
|
21 |
Ekaterinaris, J. A. and Schiff, L. B., 1993, 'Numerical Predictions of Vortical Flows over Slender Delta Wings,' J. Aircraft, Vol. 30, pp. 935-942
DOI
ScienceOn
|