-
1
-
-
0004452398
-
Quelques resultants experiment- aux sur ailes en fleche, aux faibles vitesses, obtenus en tunnel hydrodynamique
-
WERLE H. Quelques resultants experiment- aux sur ailes en fleche, aux faibles vitesses, obtenus en tunnel hydrodynamique[J]. La Recherche Aeronautique, 1954 (41): 15-21, September-October
-
(1954)
La Recherche Aeronautique
, Issue.41
, pp. 15-21
-
-
Werle, H.1
-
2
-
-
0003587703
-
Three-dimensional flow structure on delta wings at high angle-of-attack: experimental concepts and issues
-
AIAA, 93-0550
-
ROCKWELL D. Three-dimensional flow structure on delta wings at high angle-of-attack: experimental concepts and issues[R]. AIAA, 93-0550, 1993.
-
(1993)
-
-
Rockwell, D.1
-
3
-
-
0001043271
-
Survey of research on unsteady aerodynamic loading of delta wings
-
ASHLEY H, KATZ J, JARRAH M A et al. Survey of research on unsteady aerodynamic loading of delta wings[J]. Journal of Fluid and Structures, 1991, 0991(5): 363-390.
-
(1991)
Journal of Fluid and Structures
, vol.991
, Issue.5
, pp. 363-390
-
-
Ashley, H.1
Katz, J.2
Jarrah, M.A.3
-
4
-
-
3943112202
-
Vortex breakdown on slender sharp-edged Wing
-
AIAA 69-778
-
WENTZ W H J, KOHLMAN D L. Vortex breakdown on slender sharp-edged Wing[R]. AIAA 69-778, 1969.
-
(1969)
-
-
Wentz, W.H.J.1
Kohlman, D.L.2
-
5
-
-
0344786521
-
Flow studies of slender wing vortices
-
AIAA 80-1423
-
ERICHSON G E. Flow studies of slender wing vortices[R]. AIAA 80-1423, 1980.
-
(1980)
-
-
Erichson, G.E.1
-
6
-
-
22544474062
-
The effect of Reynolds number on delta wing flow
-
in Chinese
-
WANG J J, MIAO F Y, NIU Z N, XUE Q Z et al. The effect of Reynolds number on delta wing flow[J]. Journal of Experimental Mechanics, 1998, 13(4): 497-501 (in Chinese).
-
(1998)
Journal of Experimental Mechanics
, vol.13
, Issue.4
, pp. 497-501
-
-
Wang, J.J.1
Miao, F.Y.2
Niu, Z.N.3
Xue, Q.Z.4
-
7
-
-
0013306192
-
Effects of leading-edge shape and vortex burst on the flowfield of a 70° sweep delta wing
-
AIAA 89-0086
-
KEGELMAN J, ROOS F. Effects of leading-edge shape and vortex burst on the flowfield of a 70° sweep delta wing[R]. AIAA 89-0086, 1989.
-
(1989)
-
-
Kegelman, J.1
Roos, F.2
-
8
-
-
0029341383
-
Flow developments above 50° sweep delta wings with different leading-edge profiles
-
MIAU J J, KUO K T, LIU W H et al. Flow developments above 50° sweep delta wings with different leading-edge profiles[J]. Journal of Aircraft, 1995, 32(4): 787-794.
-
(1995)
Journal of Aircraft
, vol.32
, Issue.4
, pp. 787-794
-
-
Miau, J.J.1
Kuo, K.T.2
Liu, W.H.3
-
9
-
-
16244369584
-
Higher-order compact difference scheme applied to the simulation of a low sweep delta wing flow
-
AIAA, 2003-620
-
GORDNIER R E, VISBAL M R. Higher-order compact difference scheme applied to the simulation of a low sweep delta wing flow[R]. AIAA, 2003-620, 2003.
-
(2003)
-
-
Gordnier, R.E.1
Visbal, M.R.2
-
10
-
-
85085774882
-
An investigation of vortex flows over low sweep delta wings
-
AIAA, 2003-4021
-
TAYLOR G S, SCHNORBUS T, GURSUL I. An investigation of vortex flows over low sweep delta wings[R]. AIAA, 2003-4021, 2003.
-
(2003)
-
-
Taylor, G.S.1
Schnorbus, T.2
Gursul, I.3
-
11
-
-
0037273369
-
Leading-edge vortex structure of non-slender delta wings at low Reynolds number
-
Ol M V, GHARIB M. Leading-edge vortex structure of non-slender delta wings at low Reynolds number[J]. AIAA Journal, 2003, 41(1): 16-26.
-
(2003)
AIAA Journal
, vol.41
, Issue.1
, pp. 16-26
-
-
Ol, M.V.1
Gharib, M.2
-
12
-
-
25144473913
-
Effects of leading-edge bevel angle on the aerodynamic forces of a non-slender 50° delta wing
-
WANG J J, LU S F. Effects of leading-edge bevel angle on the aerodynamic forces of a non-slender 50° delta wing[J]. The Aeronautical Journal, 2005, 109(1098): 403-407.
-
(2005)
The Aeronautical Journal
, vol.109
, Issue.1098
, pp. 403-407
-
-
Wang, J.J.1
Lu, S.F.2
-
13
-
-
7544238486
-
Recent developments in delta wing aerodynamics
-
GURSUL I. Recent developments in delta wing aerodynamics[J]. The Aeronautical Journal, 2004, 108(1087): 437-45.
-
(2004)
The Aeronautical Journal
, vol.108
, Issue.1087
, pp. 437
-
-
Gursul, I.1
|