-
1
-
-
0031335568
-
Implementation of vortex wake control using SMA-actuated devices
-
T. Quackenbush, A. Bilanin, P. Batcho, R. McKilipp, B. Carpenter, Implementation of vortex wake control using SMA-actuated devices, in: Proc. SPIE, vol. 3044, 1997, pp. 134-146
-
(1997)
Proc. SPIE
, vol.3044
, pp. 134-146
-
-
Quackenbush, T.1
Bilanin, A.2
Batcho, P.3
McKilipp, R.4
Carpenter, B.5
-
2
-
-
0032686479
-
A method for accelerating the destruction of aircraft wake vortices
-
S.C. Rennich S.K. Lele A method for accelerating the destruction of aircraft wake vortices J. Aircraft 36 1999 398-404
-
(1999)
J. Aircraft
, vol.36
, pp. 398-404
-
-
Rennich, S.C.1
Lele, S.K.2
-
3
-
-
0034306752
-
Stability of a four-vortex aircraft wake model
-
D. Fabre L. Jacquin Stability of a four-vortex aircraft wake model Phys. Fluids 12 2000 2438-2443
-
(2000)
Phys. Fluids
, vol.12
, pp. 2438-2443
-
-
Fabre, D.1
Jacquin, L.2
-
4
-
-
0035311746
-
Rapidly growing instability mode in trailing multiple-vortex wakes
-
J. Ortega Ö. Savaş Rapidly growing instability mode in trailing multiple-vortex wakes AIAA J. 39 2001 750-754
-
(2001)
AIAA J.
, vol.39
, pp. 750-754
-
-
Ortega, J.1
Savaş, Ö.2
-
5
-
-
0035662527
-
Active-control system for breakup of airplane trailing vortices
-
J.D. Crouch G.D. Miller P.R. Spalart Active-control system for breakup of airplane trailing vortices AIAA J. 39 2001 2374-2381
-
(2001)
AIAA J.
, vol.39
, pp. 2374-2381
-
-
Crouch, J.D.1
Miller, G.D.2
Spalart, P.R.3
-
6
-
-
0347892206
-
Formation and structure of vortex systems generated by unflapped and flapped wing configurations
-
St. Fell R. Staufenbiel Formation and structure of vortex systems generated by unflapped and flapped wing configurations Z. Flugwiss. Weltraumforsch 19 1995 366-379
-
(1995)
Z. Flugwiss. Weltraumforsch
, vol.19
, pp. 366-379
-
-
Fell, St.1
Staufenbiel, R.2
-
7
-
-
0041437692
-
Flow field survey in the trailing vortex system behind a civil aircraft model at high lift
-
AGARD-CP-584
-
A.C. de Bruin, S.H. Hegen, P.B. Rohne, P.R. Spalart, Flow field survey in the trailing vortex system behind a civil aircraft model at high lift, AGARD-CP-584, 1996, pp. 25-1-25-12
-
(1996)
-
-
de Bruin, A.C.1
Hegen, S.H.2
Rohne, P.B.3
Spalart, P.R.4
-
8
-
-
0012468346
-
The properties of a transport aircraft wake in the extended near-field: An experimental study
-
AIAA Paper No. 2001-1038
-
L. Jacquin, D. Fabre, P. Geffroy, E. Coustols, The properties of a transport aircraft wake in the extended near-field: An experimental study, AIAA Paper No. 2001-1038, 2001
-
(2001)
-
-
Jacquin, L.1
Fabre, D.2
Geffroy, P.3
Coustols, E.4
-
10
-
-
0347555299
-
Vortex dynamics in trailing wakes of flapped rectangular wings
-
AIAA Paper No. 97-0048
-
J.D. Jacob, Ö. Savaş, Vortex dynamics in trailing wakes of flapped rectangular wings, AIAA Paper No. 97-0048, 1997
-
(1997)
-
-
Jacob, J.D.1
Savaş, Ö.2
-
11
-
-
24144477094
-
The near-far field relationship of vortices shed from transport aircraft
-
AIAA Paper No. 2001-2429
-
R. Stuff, The near-far field relationship of vortices shed from transport aircraft, AIAA Paper No. 2001-2429, 2001
-
(2001)
-
-
Stuff, R.1
-
12
-
-
24144470219
-
Wake vortex alleviation flow field studies
-
AIAA Paper No. 2004-1073
-
D.A. Durston, S.M. Walker, D.M. Driver, S.C. Smith, Ö. Savaş, Wake vortex alleviation flow field studies, AIAA Paper No. 2004-1073, 2004
-
(2004)
-
-
Durston, D.A.1
Walker, S.M.2
Driver, D.M.3
Smith, S.C.4
Savaş, Ö.5
-
13
-
-
24144462028
-
Minimized wake: A collaborative research programme on aircraft wake vortices
-
AIAA Paper No. 2003-0938
-
E. Coustols, E. Stumpf, L. Jacquin, F. Moens, H. Vollmers, T. Gerz, Minimized wake: A collaborative research programme on aircraft wake vortices, AIAA Paper No. 2003-0938, 2003
-
(2003)
-
-
Coustols, E.1
Stumpf, E.2
Jacquin, L.3
Moens, F.4
Vollmers, H.5
Gerz, T.6
-
14
-
-
24344451259
-
Numerical study of wake vortices of generic aircraft model
-
AIAA Paper No. 2001-2428
-
A. Benkenida, G. Jonville, D. Darracq, Numerical study of wake vortices of generic aircraft model, AIAA Paper No. 2001-2428, 2001
-
(2001)
-
-
Benkenida, A.1
Jonville, G.2
Darracq, D.3
-
15
-
-
24344476093
-
Numerical study of four-vortex aircraft wakes and layout of corresponding high-lift configurations
-
AIAA Paper No. 2004-1067
-
E. Stumpf, Numerical study of four-vortex aircraft wakes and layout of corresponding high-lift configurations, AIAA Paper No. 2004-1067, 2004
-
(2004)
-
-
Stumpf, E.1
-
16
-
-
0042689980
-
Two numerical studies of trailing vortices
-
AIAA Paper No. 98-0595
-
M. Shur, M. Strelets, A. Travin, P. Spalart, Two numerical studies of trailing vortices, AIAA Paper No. 98-0595, 1998
-
(1998)
-
-
Shur, M.1
Strelets, M.2
Travin, A.3
Spalart, P.4
-
17
-
-
0003471394
-
A one-equation turbulence model for aerodynamic flows
-
AIAA Paper No. 92-0439
-
P. Spalart, S.R. Allmaras, A one-equation turbulence model for aerodynamic flows, AIAA Paper No. 92-0439, 1992
-
(1992)
-
-
Spalart, P.1
Allmaras, S.R.2
-
18
-
-
0031483314
-
On the sensitization of turbulence models to rotation and curvature
-
M.L. Shur, P. Spalart, On the sensitization of turbulence models to rotation and curvature, Aerospace Sci. Technol., 1997
-
(1997)
Aerospace Sci. Technol
-
-
Shur, M.L.1
Spalart, P.2
-
19
-
-
84976552651
-
Airplane flow-field measurements
-
975535
-
J.P. Crowder, R.L. Watzlavick, T.K. Krutckoff, Airplane flow-field measurements, in: AIAA/SAE World Aviation Congress, vol. 8 (975535), 1997, pp. 1-9
-
(1997)
AIAA/SAE World Aviation Congress
, vol.8
, pp. 1-9
-
-
Crowder, J.P.1
Watzlavick, R.L.2
Krutckoff, T.K.3
-
20
-
-
0042727087
-
An upwind differencing scheme for the time-accurate incompressible Navier-Stokes equations
-
AIAA Paper No. 88-2583-CP
-
S.E. Rogers, D. Kwak, An upwind differencing scheme for the time-accurate incompressible Navier-Stokes equations, AIAA Paper No. 88-2583-CP, 1988
-
(1988)
-
-
Rogers, S.E.1
Kwak, D.2
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