Effects of leading-edge bevel angle on the aerodynamic forces of a non-slender 50° delta wing.
- Published in:
- Aeronautical Journal, 2005, v. 109, n. 1098, p. 403, doi. 10.1017/S0001924000000828
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- Publication type:
- Article
Works matching DE "AIRPLANE triangular wings"
Results: 15
1
2
Wind-tunnel interference effects on a 70° delta wing.
- Published in:
- Aeronautical Journal, 2004, v. 108, n. 1088, p. 505, doi. 10.1017/S0001924000000336
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- Publication type:
- Article
3
Vortex breakdown location over 65° delta wings empiricism and experiment.
- Published in:
- Aeronautical Journal, 2004, v. 108, n. 1087, p. 475, doi. 10.1017/S0001924000000294
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- Publication type:
- Article
4
Recent developments in delta wing aerodynamics.
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- Aeronautical Journal, 2004, v. 108, n. 1087, p. 437, doi. 10.1017/S0001924000000269
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- Publication type:
- Article
5
A Comparative Study of the Enhancement of Heat Transfer by Delta Wing Vortex Generators and V Shaped Dimples Using Experimentation and CFD.
- Published in:
- International Review of Mechanical Engineering, 2017, v. 11, n. 10, p. 769, doi. 10.15866/ireme.v11i10.12898
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- Publication type:
- Article
6
Computation of Stiffness derivative for an unsteady delta wing with curved leading edges.
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- International Journal of Recent Research Aspects, 2017, v. 4, n. 4, p. 69
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- Article
7
Effect of Pitching Delta Wing on Vortex Structures with and without Impingement Plate.
- Published in:
- Turkish Journal of Engineering & Environmental Sciences, 2002, v. 26, n. 4, p. 325
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- Publication type:
- Article
8
COMPUTATIONAL AND ANALYTICAL INVESTIGATION OF AERODYNAMIC DERIVATIVES OF SIMILITUDE DELTA WING MODEL AT HYPERSONIC SPEEDS.
- Published in:
- International Journal of Technology, 2017, v. 8, n. 3, p. 366, doi. 10.14716/ijtech.v8i3.6319
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- Article
9
Computation of field structure and aerodynamic characteristics of delta wings at high angles of attack.
- Published in:
- Applied Mathematics & Mechanics, 2005, v. 26, n. 6, p. 797, doi. 10.1007/BF02465431
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- Article
10
Research on the hysteresis properties of unsteady aerodynamics about the oscillating wings.
- Published in:
- Applied Mathematics & Mechanics, 1999, v. 20, n. 8, p. 895, doi. 10.1007/BF02452488
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- Article
11
Distinctive Features of Flow in the Hypersonic Boundary Layer in the Vicinity of the Plane of Symmetry of a Planar Wing Having a Bend of the Leading Edge.
- Published in:
- Fluid Dynamics, 2019, v. 54, n. 4, p. 472, doi. 10.1134/S0015462819030030
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- Publication type:
- Article
12
Propagation of perturbations in the three-dimensional boundary layer on a delta wing in the viscid-inviscid interaction regime.
- Published in:
- Fluid Dynamics, 2010, v. 45, n. 3, p. 422, doi. 10.1134/S0015462810030099
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- Article
13
Formation of Supercritical Flow Regions on Low-Aspect-Ratio Wings.
- Published in:
- Fluid Dynamics, 2005, v. 40, n. 6, p. 973, doi. 10.1007/s10697-006-0012-4
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- Article
14
A Limiting Solution for Flow Past a Delta Wing in the Presence of Supercritical Flow Regions.
- Published in:
- Fluid Dynamics, 2002, v. 37, n. 6, p. 939, doi. 10.1023/A:1022308615249
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- Publication type:
- Article
15
EXPERIMENTAL INVESTIGATION ON A PITCHING MOTION DELTA WING IN UNSTEADY FREE STREAM.
- Published in:
- Modern Physics Letters B, 2009, v. 23, n. 3, p. 409, doi. 10.1142/S0217984909018527
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- Publication type:
- Article