-
1
-
-
0022075426
-
The discrete vortices from a delta wing
-
GAD-EL-HAK, M. and BLACKWELDER, R.F. The discrete vortices from a delta wing, AIAA J, 1985, 23, pp 961-962.
-
(1985)
AIAA J
, vol.23
, pp. 961-962
-
-
Gad-El-Hak, M.1
Blackwelder, R.F.2
-
2
-
-
0542369447
-
Development of a three-dimensional free shear layer
-
RILEY, A.J. and LOWSON, M.V. Development of a three-dimensional free shear layer, J Fluid Mechanics, 1998, 369, pp 49-89.
-
(1998)
J Fluid Mechanics
, vol.369
, pp. 49-89
-
-
Riley, A.J.1
Lowson, M.V.2
-
3
-
-
0036684210
-
Vortical substructures in the shear layers forming leading-edge vortices
-
MITCHELL, A.M. and MOLTON, P. Vortical substructures in the shear layers forming leading-edge vortices, AIAA J, 2002, 40, (8), pp 1689-1692.
-
(2002)
AIAA J
, vol.40
, Issue.8
, pp. 1689-1692
-
-
Mitchell, A.M.1
Molton, P.2
-
4
-
-
84897738927
-
Computational and physical aspects of UAV vortical flows
-
4-5 November, University of Bath, UK
-
VISBAL, M.R. Computational and physical aspects of UAV vortical flows, Workshop on aerodynamic issues of unmanned air vehicles, 4-5 November 2002, University of Bath, UK. See also, VISBAL, M.R. and GORDNIER, R.E., On the structure of the shear layer emanating from a swept leading edge at angle-of-attack, AIAA-2003-4016, 33rd Fluid dynamics conference and exhibit, 23-26 June 2003, Orlando, FL, USA.
-
(2002)
Workshop on Aerodynamic Issues of Unmanned Air Vehicles
-
-
Visbal, M.R.1
-
5
-
-
84894622644
-
On the structure of the shear layer emanating from a swept leading edge at angle-of-attack
-
AIAA-2003-4016, 23-26 June, Orlando, FL, USA
-
VISBAL, M.R. Computational and physical aspects of UAV vortical flows, Workshop on aerodynamic issues of unmanned air vehicles, 4-5 November 2002, University of Bath, UK. See also, VISBAL, M.R. and GORDNIER, R.E., On the structure of the shear layer emanating from a swept leading edge at angle-of-attack, AIAA-2003-4016, 33rd Fluid dynamics conference and exhibit, 23-26 June 2003, Orlando, FL, USA.
-
(2003)
33rd Fluid Dynamics Conference and Exhibit
-
-
Visbal, M.R.1
Gordnier, R.E.2
-
7
-
-
0021500558
-
Vortex stability and breakdown: Survey and extension
-
LEIBOVICH, S. Vortex stability and breakdown: survey and extension, AIAA J, 1984, 22, (9), pp 1192-1206.
-
(1984)
AIAA J
, vol.22
, Issue.9
, pp. 1192-1206
-
-
Leibovich, S.1
-
9
-
-
85039479798
-
High resolution computational unsteady aerodynamic techniques applied to maneuvering unmanned combat aircraft
-
4-5 November, University of Bath, UK
-
MORTON, S. High resolution computational unsteady aerodynamic techniques applied to maneuvering unmanned combat aircraft, workshop on aerodynamic issues of unmanned air vehicles, 4-5 November 2002, University of Bath, UK. See also, CEAS Aerospace Aerodynamics Research Conference, 10-12 June 2003, London, UK.
-
(2002)
Workshop on Aerodynamic Issues of Unmanned Air Vehicles
-
-
Morton, S.1
-
10
-
-
85039479405
-
-
10-12 June, London, UK
-
MORTON, S. High resolution computational unsteady aerodynamic techniques applied to maneuvering unmanned combat aircraft, workshop on aerodynamic issues of unmanned air vehicles, 4-5 November 2002, University of Bath, UK. See also, CEAS Aerospace Aerodynamics Research Conference, 10-12 June 2003, London, UK.
-
(2003)
CEAS Aerospace Aerodynamics Research Conference
-
-
-
12
-
-
85039468046
-
Aspects of use of CFD for configuration design of UAV concepts
-
4-5 November, University of Bath, UK
-
PEMBERTON, T. Aspects of use of CFD for configuration design of UAV concepts, Workshop on aerodynamic issues of unmanned air vehicles. 4-5 November 2002, University of Bath, UK.
-
(2002)
Workshop on Aerodynamic Issues of Unmanned Air Vehicles
-
-
Pemberton, T.1
-
13
-
-
0028378145
-
Unsteady flow phenomena over delta wings at high angle-of-attack
-
February
-
GURSUL, I. Unsteady flow phenomena over delta wings at high angle-of-attack, AIAA J, February 1994, 32, (2), pp 225-231.
-
(1994)
AIAA J
, vol.32
, Issue.2
, pp. 225-231
-
-
Gursul, I.1
-
14
-
-
0032710775
-
Buffeting flows over delta wings
-
GURSUL, I. and XIE, W. Buffeting flows over delta wings, AIM J, 1999, 37, (1), pp 58-65.
-
(1999)
AIM J
, vol.37
, Issue.1
, pp. 58-65
-
-
Gursul, I.1
Xie, W.2
-
15
-
-
0031467180
-
Unsteady nature of leading edge vortices
-
MENKE, M. and GURSUL, I. Unsteady nature of leading edge vortices, Physics of Fluids, 1997, 9, (10), pp 1-7.
-
(1997)
Physics of Fluids
, vol.9
, Issue.10
, pp. 1-7
-
-
Menke, M.1
Gursul, I.2
-
16
-
-
85067321251
-
Review of unsteady vortex flows over slender delta wings
-
in print
-
GURSUL, I. Review of unsteady vortex flows over slender delta wings, J Aircr, in print. See also, AIAA-2003-3942, AIAA Applied Aerodynamics Conference, 23-26 June, 2003, Orlando, FL, USA.
-
J Aircr
-
-
Gursul, I.1
-
17
-
-
85067321251
-
-
AIAA-2003-3942, 23-26 June, Orlando, FL, USA
-
GURSUL, I. Review of unsteady vortex flows over slender delta wings, J Aircr, in print. See also, AIAA-2003-3942, AIAA Applied Aerodynamics Conference, 23-26 June, 2003, Orlando, FL, USA.
-
(2003)
AIAA Applied Aerodynamics Conference
-
-
-
18
-
-
0032592744
-
Experiments on the unsteady nature of vortex breakdown over delta wings
-
MENKE, M., YANG, H. and GURSUL, I. Experiments on the unsteady nature of vortex breakdown over delta wings, Experiments in Fluids, 1999, 27, (3), pp 262-272.
-
(1999)
Experiments in Fluids
, vol.27
, Issue.3
, pp. 262-272
-
-
Menke, M.1
Yang, H.2
Gursul, I.3
-
19
-
-
1942460751
-
Aeroelastic response of a flexible delta wing due to unsteady vortex flows
-
AIAA-2003-1106, 6-9 January, Reno, NV, USA
-
GRAY, J.M., GURSUL, I. and BUTLER, R. Aeroelastic response of a flexible delta wing due to unsteady vortex flows, AIAA-2003-1106, 41st Aerospace Sciences Meeting and Exhibit, 6-9 January 2003, Reno, NV, USA.
-
(2003)
41st Aerospace Sciences Meeting and Exhibit
-
-
Gray, J.M.1
Gursul, I.2
Butler, R.3
-
20
-
-
85085774882
-
An investigation of vortex flows over low sweep delta wings
-
AIAA-2003-4021, 23-26 June, Orlando, FL, USA
-
TAYLOR, G., SCHNORBUS, T. and GURSUL, I. An investigation of vortex flows over low sweep delta wings, AIAA-2003-4021, AIAA Fluid Dynamics Conference, 23-26 June 2003, Orlando, FL, USA.
-
(2003)
AIAA Fluid Dynamics Conference
-
-
Taylor, G.1
Schnorbus, T.2
Gursul, I.3
-
21
-
-
12844270349
-
Higher-order compact difference scheme applied to the simulation of a low sweep delta wing flow
-
AIAA-2003-0620, 6-9 January, Reno, NV, USA
-
GORDNIER, R.E. and Visbal, M.R. Higher-order compact difference scheme applied to the simulation of a low sweep delta wing flow, AIAA-2003-0620, 41st Aerospace Sciences Meeting and Exhibit, 6-9 January 2003, Reno, NV, USA.
-
(2003)
41st Aerospace Sciences Meeting and Exhibit
-
-
Gordnier, R.E.1
Visbal, M.R.2
-
22
-
-
84894308360
-
Self-induced roll oscillation of 45-degree delta wing
-
AIAA-2000-0655, 10-13 January, Reno, NV, USA
-
MATSUNO, T. and NAKAMURA, Y. Self-induced roll oscillation of 45-degree delta wing, AIAA-2000-0655, 38th AIAA Aerospace Sciences Meeting and Exhibit, 10-13 January 2000, Reno, NV, USA.
-
(2000)
38th AIAA Aerospace Sciences Meeting and Exhibit
-
-
Matsuno, T.1
Nakamura, Y.2
-
23
-
-
0022161641
-
The pitching delta wing
-
GAD-EL-HAK, M. and Ho, C.M. The pitching delta wing, AIAA J, 1985, 23, (11), pp 1660-1665.
-
(1985)
AIAA J
, vol.23
, Issue.11
, pp. 1660-1665
-
-
Gad-El-Hak, M.1
Ho, C.M.2
-
24
-
-
0003339740
-
Three-dimensional flow structure on delta wings at high angle-of-attack: Experimental concepts and issues
-
January
-
ROCKWELL, D. Three-dimensional flow structure on delta wings at high angle-of-attack: experimental concepts and issues, AIAA Paper 93-0550, January 1993.
-
(1993)
AIAA Paper
, vol.93
, Issue.550
-
-
Rockwell, D.1
-
25
-
-
33845785586
-
Computational and physical aspects of vortex breakdown on delta wings
-
January
-
VISBAL, M.R. Computational and physical aspects of vortex breakdown on delta wings, AIAA Paper 95-0585, January 1995.
-
(1995)
AIAA Paper
, vol.95
, Issue.585
-
-
Visbal, M.R.1
-
26
-
-
0034226218
-
Proposed mechanism for time lag of vortex breakdown location in unsteady flows
-
GURSUL, I. Proposed mechanism for time lag of vortex breakdown location in unsteady flows, J Aircr, 2000, 37, (4), pp 733-736.
-
(2000)
J Aircr
, vol.37
, Issue.4
, pp. 733-736
-
-
Gursul, I.1
-
27
-
-
0035613410
-
High-fidelity computational simulation of nonlinear fluid-structure interaction problems
-
4-5 November, University of Bath, UK
-
GORDNIER, R. High-fidelity computational simulation of nonlinear fluid-structure interaction problems, workshop on aerodynamic issues of unmanned air vehicles, 4-5 November 2002, University of Bath, UK. See also, GORDNIER, R. and MELVILLE, R., Numerical simulation of limit-cycle oscillations of a cropped delta wing using the full navier-stokes equations, Int J Computational Fluid Dynamics, 2001, 14, (3), pp 211-224.
-
(2002)
Workshop on Aerodynamic Issues of Unmanned Air Vehicles
-
-
Gordnier, R.1
-
28
-
-
0035613410
-
Numerical simulation of limit-cycle oscillations of a cropped delta wing using the full navier-stokes equations
-
GORDNIER, R. High-fidelity computational simulation of nonlinear fluid-structure interaction problems, workshop on aerodynamic issues of unmanned air vehicles, 4-5 November 2002, University of Bath, UK. See also, GORDNIER, R. and MELVILLE, R., Numerical simulation of limit-cycle oscillations of a cropped delta wing using the full navier-stokes equations, Int J Computational Fluid Dynamics, 2001, 14, (3), pp 211-224.
-
(2001)
Int J Computational Fluid Dynamics
, vol.14
, Issue.3
, pp. 211-224
-
-
Gordnier, R.1
Melville, R.2
-
29
-
-
4944222327
-
Buffeting flows over a low sweep delta wing
-
September
-
TAYLOR, G.S. and GURSUL, I. Buffeting flows over a low sweep delta wing, AIAA J, September 2004, 42, (9), pp 1737-1745. See also, Unsteady vortex flows and buffeting of a low sweep delta wing, AIAA-2004-106, 42nd Aerospace Sciences Meeting and Exhibit, 5-8 January 2004, Reno, NV.
-
(2004)
AIAA J
, vol.42
, Issue.9
, pp. 1737-1745
-
-
Taylor, G.S.1
Gursul, I.2
-
30
-
-
4944222327
-
Unsteady vortex flows and buffeting of a low sweep delta wing
-
AIAA-2004-106, 5-8 January, Reno, NV
-
TAYLOR, G.S. and GURSUL, I. Buffeting flows over a low sweep delta wing, AIAA J, September 2004, 42, (9), pp 1737-1745. See also, Unsteady vortex flows and buffeting of a low sweep delta wing, AIAA-2004-106, 42nd Aerospace Sciences Meeting and Exhibit, 5-8 January 2004, Reno, NV.
-
(2004)
42nd Aerospace Sciences Meeting and Exhibit
-
-
-
31
-
-
85088721748
-
Lift enhancement over a flexible delta wing
-
AIAA-2004-2618, June 2004, Portland, Oregon
-
TAYLOR, G.S. and GURSUL, I. Lift enhancement over a flexible delta wing, AIAA-2004-2618, 2nd AIAA Flow Control Conference, June 2004, Portland, Oregon.
-
2nd AIAA Flow Control Conference
-
-
Taylor, G.S.1
Gursul, I.2
-
32
-
-
0038543098
-
Effect of a trailing-edge jet on fin buffeting
-
PHILLIPS, S., LAMBERT, C. and GURSUL, I. Effect of a trailing-edge jet on fin buffeting, J Aircr, 2003, 40, (3), pp 590-599.
-
(2003)
J Aircr
, vol.40
, Issue.3
, pp. 590-599
-
-
Phillips, S.1
Lambert, C.2
Gursul, I.3
-
33
-
-
85039471087
-
Membrane wing aerodynamics for MAV applications
-
4-5 November, University of Bath, UK
-
SHYY, W. Membrane wing aerodynamics for MAV applications, workshop on aerodynamic issues of unmanned air vehicles, 4-5 November 2002, University of Bath, UK.
-
(2002)
Workshop on Aerodynamic Issues of Unmanned Air Vehicles
-
-
Shyy, W.1
-
34
-
-
0030479114
-
4
-
September
-
4, AIAA J, September 1996, 34, (9), pp 1941-1942.
-
(1996)
AIAA J
, vol.34
, Issue.9
, pp. 1941-1942
-
-
Laitone, E.V.1
-
35
-
-
85088720830
-
Vortex flows over fixed-wing micro air vehicles
-
AIAA-2002-0698, 14-17 January, Reno, NV, USA
-
GURSUL, I., TAYLOR, G. and WOODING, C.L. Vortex flows over fixed-wing micro air vehicles, AIAA-2002-0698, 40th AIAA Aerospace Meeting and Exhibit, 14-17 January 2002, Reno, NV, USA.
-
(2002)
40th AIAA Aerospace Meeting and Exhibit
-
-
Gursul, I.1
Taylor, G.2
Wooding, C.L.3
-
36
-
-
0003232284
-
Aerodynamic characteristics of low aspect ratio wings at low reynolds numbers
-
Univ of Notre Dame, Notre Dame, IN, 5-7 June
-
TORRES, G.E. and MUELLER, T.J. Aerodynamic characteristics of low aspect ratio wings at low reynolds numbers, Proceedings of the conference: Fixed, flapping and rotary wing vehicles at very low Reynolds Numbers, Univ of Notre Dame, Notre Dame, IN, 5-7 June 2000, pp 228-305.
-
(2000)
Proceedings of the Conference: Fixed, Flapping and Rotary Wing Vehicles at Very Low Reynolds Numbers
, pp. 228-305
-
-
Torres, G.E.1
Mueller, T.J.2
-
37
-
-
0012574236
-
Reynolds number effects on the vortical-flow structure generated by a double-delta wing
-
HEBBAR, S.K., PLATZER, M.F. and FRITZELAS, A.E. Reynolds number effects on the vortical-flow structure generated by a double-delta wing, Experiments in fluids, 2000, 28, pp 206-216.
-
(2000)
Experiments in Fluids
, vol.28
, pp. 206-216
-
-
Hebbar, S.K.1
Platzer, M.F.2
Fritzelas, A.E.3
-
38
-
-
0032592965
-
Flapping and flexible wings for biological and micro air vehicles
-
SHYY, W., BERG, M. and LJUNGQVIST, D. Flapping and flexible wings for biological and micro air vehicles, Progress in Aerospace Sciences, 1999, 35, pp 455-505.
-
(1999)
Progress in Aerospace Sciences
, vol.35
, pp. 455-505
-
-
Shyy, W.1
Berg, M.2
Ljungqvist, D.3
-
40
-
-
0000845062
-
-
ed. Wu, Y-T, BROKAW, C.J. and BRENNEN, C. New York/London:Plenum
-
LIGHTHILL, M.J. Aerodynamic Aspects of Animal Flight, in Swimming and Flying in Nature, 2, ed. Wu, Y-T, BROKAW, C.J. and BRENNEN, C. pp 423-491. New York/London:Plenum, 1975.
-
(1975)
Aerodynamic Aspects of Animal Flight, in Swimming and Flying in Nature
, vol.2
, pp. 423-491
-
-
Lighthill, M.J.1
-
41
-
-
0042176897
-
Aerodynamics of small vehicles
-
MUELLER, T.J. and DELAURIER, J.D. Aerodynamics of small vehicles, Annual Review of Fluid Mechanics, 2003, 35, pp 89-111.
-
(2003)
Annual Review of Fluid Mechanics
, vol.35
, pp. 89-111
-
-
Mueller, T.J.1
Delaurier, J.D.2
-
42
-
-
0019399231
-
The fluid dynamics of insect flight
-
MAXWORTHY, T. The fluid dynamics of insect flight, Annual Review of Fluid Mechanics, 1981, 13, pp 329-350.
-
(1981)
Annual Review of Fluid Mechanics
, vol.13
, pp. 329-350
-
-
Maxworthy, T.1
-
44
-
-
85085779281
-
Flapping wing propulsion for a micro air vehicle
-
AIAA-2000-0897, 10-13 January, Reno, NV
-
JONES, K.D. and PLATZER, M.F. Flapping wing propulsion for a micro air vehicle, AIAA-2000-0897, 38th Aerospace Sciences Meeting and Exhibit, 10-13 January 2000, Reno, NV.
-
(2000)
38th Aerospace Sciences Meeting and Exhibit
-
-
Jones, K.D.1
Platzer, M.F.2
-
45
-
-
0000183758
-
Experimental and computational investigation of the Knoller-Betz effect
-
May
-
JONES, K.D., DOHRING, C.M. and PLATZER, M.F. Experimental and Computational Investigation of the Knoller-Betz Effect, AIAA J, May 1998, 36, (7), pp 1240-1246.
-
(1998)
AIAA J
, vol.36
, Issue.7
, pp. 1240-1246
-
-
Jones, K.D.1
Dohring, C.M.2
Platzer, M.F.3
-
46
-
-
3042538591
-
Experimental and computational investigation of flapping wing propulsion for micro air vehicles
-
Chapter 16 in, MUELLER, T.J. (Ed), published by AIAA
-
JONES, K.D., LUND, T.C. and PLATZER, M.F. Experimental and computational investigation of flapping wing propulsion for micro air vehicles, Chapter 16 in Fixed and Flapping Wing Aerodynamics for Micro air Vehicle Applications, MUELLER, T.J. (Ed) pp 307-339, published by AIAA, 2001.
-
(2001)
Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications
, pp. 307-339
-
-
Jones, K.D.1
Lund, T.C.2
Platzer, M.F.3
-
47
-
-
9744240934
-
Flexible flapping airfoil propulsion at zero freestream velocity
-
November
-
HEATHCOTE, S., MARTIN, D. and GURSUL, I., flexible flapping airfoil propulsion at zero freestream velocity, AIAA J, November 2004, 42, (11), pp 2196-2204. See also, AIAA-2003-3446, AIAA Fluid Dynamics Conference, 23-26 June 2003, Orlando, FL.
-
(2004)
AIAA J
, vol.42
, Issue.11
, pp. 2196-2204
-
-
Heathcote, S.1
Martin, D.2
Gursul, I.3
-
48
-
-
9744240934
-
-
AIAA-2003-3446, 23-26 June, Orlando, FL
-
HEATHCOTE, S., MARTIN, D. and GURSUL, I., flexible flapping airfoil propulsion at zero freestream velocity, AIAA J, November 2004, 42, (11), pp 2196-2204. See also, AIAA-2003-3446, AIAA Fluid Dynamics Conference, 23-26 June 2003, Orlando, FL.
-
(2003)
AIAA Fluid Dynamics Conference
-
-
-
49
-
-
84885330053
-
Aerodynamics and propulsion of synthetic jet based micro air vehicles
-
AIAA-2003-4004, 23-26 June, Orlando, FL
-
WHITEHEAD, J. and GURSUL, I. Aerodynamics and propulsion of synthetic jet based micro air vehicles, AIAA-2003-4004, AIAA Fluid Dynamics Conference, 23-26 June, 2003, Orlando, FL.
-
(2003)
AIAA Fluid Dynamics Conference
-
-
Whitehead, J.1
Gursul, I.2
-
50
-
-
2942705825
-
Interaction of synthetic jet propulsion with wing aerodynamics at low reynolds numbers
-
AIAA-2004-0093, 3-8 January, Reno, Nevada
-
WHITEHEAD, J. and GURSUL, I. Interaction of synthetic jet propulsion with wing aerodynamics at low reynolds numbers, AIAA-2004-0093, 42nd Aeropsace Sciences Meeting and Exhibit 3-8 January 2004, Reno, Nevada.
-
(2004)
42nd Aeropsace Sciences Meeting and Exhibit
-
-
Whitehead, J.1
Gursul, I.2
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