-
2
-
-
10944244891
-
-
SAAB Aktiebolag, TN 60, Linkoeping, Sweden
-
Behrbohm, H., "Basic Low Speed Aerodynamics of the Short-Coupled Canard Configuration of Small Aspect Ratio," SAAB Aktiebolag, TN 60, Linkoeping, Sweden, 1965.
-
(1965)
Basic Low Speed Aerodynamics of the Short-Coupled Canard Configuration of Small Aspect Ratio
-
-
Behrbohm, H.1
-
3
-
-
11644285533
-
Vortex Interference Effects on Close-Coupled Canard Configuration at Low Speed
-
AGARD
-
Hummel, D., and Oelker H.-C., "Vortex Interference Effects on Close-Coupled Canard Configuration at Low Speed," Aerodynamics of Combat Aircraft Controls and of Ground Effects, CP-465, AGARD, 1989, pp. 7-1-7-18.
-
(1989)
Aerodynamics of Combat Aircraft Controls and of Ground Effects
, vol.CP-465
, pp. 71-718
-
-
Hummel, D.1
Oelker, H.-C.2
-
4
-
-
85036708921
-
Vortex Formation over a Close-Coupled Canard-Wing-Body Configuration in Unsymmetrical Flow
-
AGARD
-
Bergmann, Á., Hummel, D., and Oelker H.-C., "Vortex Formation over a Close-Coupled Canard-Wing-Body Configuration in Unsymmetrical Flow," Vortex Flow Aerodynamics, CP-494, AGARD, 1990, pp. 1-14.
-
(1990)
Vortex Flow Aerodynamics
, vol.CP-494
, pp. 1-14
-
-
Bergmann, Á.1
Hummel, D.2
Oelker, H.-C.3
-
5
-
-
85002640940
-
-
AIAA Paper 86-2179, Aug.
-
Ying, S. X., Steger, J. L., Schiff, L. B., and Baganoff, D., "Numerical Simulation of Unsteady, Viscous High-Angle-of-Attack Flows Using a Partially Flux-Split Algorithm," AIAA Paper 86-2179, Aug. 1986.
-
(1986)
Numerical Simulation of Unsteady, Viscous High-Angle-of-Attack Flows Using a Partially Flux-Split Algorithm
-
-
Ying, S.X.1
Steger, J.L.2
Schiff, L.B.3
Baganoff, D.4
-
6
-
-
0026923001
-
Navier-Stokes Simulation of a Close-Coupled Canard-Wing-Body Configuration
-
Tu, E. L., "Navier-Stokes Simulation of a Close-Coupled Canard-Wing-Body Configuration," Journal of Aircraft, Vol. 29, No. 5, 1992, pp. 830-838.
-
(1992)
Journal of Aircraft
, vol.29
, Issue.5
, pp. 830-838
-
-
Tu, E.L.1
-
7
-
-
0028192741
-
Effect of Canard Deflection on Close-Coupled Canard-Wing-Body Aerodynamics
-
Tu, E. L., "Effect of Canard Deflection on Close-Coupled Canard-Wing-Body Aerodynamics" Journal of Aircraft, Vol. 31, No. 1, 1994, pp. 138-145.
-
(1994)
Journal of Aircraft
, vol.31
, Issue.1
, pp. 138-145
-
-
Tu, E.L.1
-
8
-
-
0029306348
-
Analysis of Flowfields over Missile Configurations at Subsonic Speeds
-
Ekaterinaris, J. A., "Analysis of Flowfields over Missile Configurations at Subsonic Speeds," Journal of Spacecraft and Rockets, Vol. 32, No. 3, 1995, pp. 385-391.
-
(1995)
Journal of Spacecraft and Rockets
, vol.32
, Issue.3
, pp. 385-391
-
-
Ekaterinaris, J.A.1
-
9
-
-
84889179530
-
-
AIAA Paper 95-1863, June
-
Gutmark, E. J., Yu, K., VanDyken, R. D., Tuncer, I. H., and McLachlan, B. G., "Experimental and Computational Study of Canard-Wing-Body Configuration at High Angle-of-Attack," AIAA Paper 95-1863, June 1995.
-
(1995)
Experimental and Computational Study of Canard-Wing-Body Configuration at High Angle-of-Attack
-
-
Gutmark, E.J.1
Yu, K.2
VanDyken, R.D.3
Tuncer, I.H.4
McLachlan, B.G.5
-
10
-
-
84889170216
-
-
AIAA Paper 96-0661, Jan.
-
VanDyken, R. D., Gutmark, E. J., Yu, K., Tuncer, I. H., Platzer. M. F., and McLachlan, B. G., "Passive and Active Control of Flow Separation over Delta Wings at High Angle-of-Attack," AIAA Paper 96-0661, Jan. 1996.
-
(1996)
Passive and Active Control of Flow Separation over Delta Wings at High Angle-of-Attack
-
-
VanDyken, R.D.1
Gutmark, E.J.2
Yu, K.3
Tuncer, I.H.4
Platzer, M.F.5
McLachlan, B.G.6
-
11
-
-
84889169300
-
-
AIAA Paper 96-0189, Jan.
-
Tuncer, I. H., Marvin, R., and Platzer, M. F., "Numerical Investigation of Subsonic Flow over a Typical Missile Forebody," AIAA Paper 96-0189, Jan. 1996.
-
(1996)
Numerical Investigation of Subsonic Flow over a Typical Missile Forebody
-
-
Tuncer, I.H.1
Marvin, R.2
Platzer, M.F.3
-
12
-
-
84889173292
-
-
AIAA Paper 97-0635, Jan.
-
Tuncer, I. H., Platzer, M. F., and VanDyken, R. D., "A Computational Study of Subsonic Flowfields over a Missile Configuration," AIAA Paper 97-0635, Jan. 1997.
-
(1997)
A Computational Study of Subsonic Flowfields over a Missile Configuration
-
-
Tuncer, I.H.1
Platzer, M.F.2
VanDyken, R.D.3
-
14
-
-
11644258331
-
-
AIAA Paper 92-2686, June
-
McLachlan, B. G., Bell, J. H., Kennelly, R. A., Schreiner, J. A., Smith, S. C., and Strong, J. M., "Pressure Sensitive Paint Use in the Supersonic High-Sweep Oblique Wing Test," AIAA Paper 92-2686, June 1992.
-
(1992)
Pressure Sensitive Paint Use in the Supersonic High-Sweep Oblique Wing Test
-
-
McLachlan, B.G.1
Bell, J.H.2
Kennelly, R.A.3
Schreiner, J.A.4
Smith, S.C.5
Strong, J.M.6
|