-
1
-
-
0021600203
-
Practical computation of unsteady lift
-
Beddoes T.S. Practical computation of unsteady lift. Vertica. 8:1984;55-71.
-
(1984)
Vertica
, vol.8
, pp. 55-71
-
-
Beddoes, T.S.1
-
3
-
-
0035997576
-
Active wing flutter suppression using a trailing edge flap
-
Borglund D., Kuttenkeuler J. Active wing flutter suppression using a trailing edge flap. J. Fluids and Structures. 16:2002;271-294.
-
(2002)
J. Fluids and Structures
, vol.16
, pp. 271-294
-
-
Borglund, D.1
Kuttenkeuler, J.2
-
4
-
-
0039926999
-
Adaptive blade twist - Calculations and experimental results
-
Büter A., Breitbach E. Adaptive blade twist - calculations and experimental results. Aerosp. Sci. Technol. 4:2000;309-319.
-
(2000)
Aerosp. Sci. Technol.
, vol.4
, pp. 309-319
-
-
Büter, A.1
Breitbach, E.2
-
5
-
-
0032757223
-
Renaissance of aeroelasticity and its future
-
Friedmann P.P. Renaissance of aeroelasticity and its future. J. Aircraft. 36:1999;105-121.
-
(1999)
J. Aircraft
, vol.36
, pp. 105-121
-
-
Friedmann, P.P.1
-
6
-
-
0030247268
-
Unsteady aerodynamics of a flapped airfoil in subsonic flow by indicial concepts
-
Hariharan N., Leishman J.G. Unsteady aerodynamics of a flapped airfoil in subsonic flow by indicial concepts. J. Aircraft. 33:1996;855-868.
-
(1996)
J. Aircraft
, vol.33
, pp. 855-868
-
-
Hariharan, N.1
Leishman, J.G.2
-
8
-
-
0024088694
-
Validation of approximate indical aerodynamic functions for two-dimensional subsonic flow
-
Leishman J.G. Validation of approximate indical aerodynamic functions for two-dimensional subsonic flow. J. Aircraft. 25:1988;914-922.
-
(1988)
J. Aircraft
, vol.25
, pp. 914-922
-
-
Leishman, J.G.1
-
10
-
-
0025429297
-
A state-space representation of unsteady aerodynamic behaviour
-
Leishman J.G., Nguyen K.O. A state-space representation of unsteady aerodynamic behaviour. AIAA J. 28:1990;836-845.
-
(1990)
AIAA J.
, vol.28
, pp. 836-845
-
-
Leishman, J.G.1
Nguyen, K.O.2
-
11
-
-
0030245368
-
Open- and closed-loop results of a strain-actuated active aeroelastic wing
-
Lin C.Y., Crawley E.F., Heeg J. Open- and closed-loop results of a strain-actuated active aeroelastic wing. J. Aircraft. 33:1996;987-994.
-
(1996)
J. Aircraft
, vol.33
, pp. 987-994
-
-
Lin, C.Y.1
Crawley, E.F.2
Heeg, J.3
-
13
-
-
1842491550
-
Unsteady incompressible potential flow around an airfoil with variable camber
-
Mesarič M., Kosel F. Unsteady incompressible potential flow around an airfoil with variable camber. Proceedings Kuhljevi dnevi '02. 2002;73-80.
-
(2002)
Proceedings Kuhljevi dnevi '02
, pp. 73-80
-
-
Mesarič, M.1
Kosel, F.2
-
14
-
-
1842543654
-
Active control of the aeroelastic response of an airfoil
-
Mesarič M., Kosel F. Active control of the aeroelastic response of an airfoil. Proceedings Kuhljevi dnevi '03. 2003;17-24.
-
(2003)
Proceedings Kuhljevi dnevi '03
, pp. 17-24
-
-
Mesarič, M.1
Kosel, F.2
-
15
-
-
0035599181
-
Realization of an optimized wing camber by using formvariable flap structures
-
Monner H.P. Realization of an optimized wing camber by using formvariable flap structures. Aerosp. Sci. Technol. 5:2001;445-455.
-
(2001)
Aerosp. Sci. Technol.
, vol.5
, pp. 445-455
-
-
Monner, H.P.1
-
16
-
-
0029728210
-
Controled aeroelastic response and airfoil shaping using adaptive materials and integrated systems
-
San Diego
-
Pinkerton J.L., McGowan A.R., Moses R.W., Scott R.C., Hegg J. Controled aeroelastic response and airfoil shaping using adaptive materials and integrated systems. SPIE's 1996 Symposium on Smart Structures and Integrated Systems, San Diego. 1996.
-
(1996)
SPIE's 1996 Symposium on Smart Structures and Integrated Systems
-
-
Pinkerton, J.L.1
Mcgowan, A.R.2
Moses, R.W.3
Scott, R.C.4
Hegg, J.5
-
17
-
-
0035472772
-
Adaptive wing and flow control technology
-
Stanewsky E. Adaptive wing and flow control technology. Progr. Aerospace Sci. 37:2001;583-667.
-
(2001)
Progr. Aerospace Sci.
, vol.37
, pp. 583-667
-
-
Stanewsky, E.1
-
18
-
-
0003927402
-
General theory of aerodynamic instability and the mechanism of flutter
-
T. Theodorsen, General theory of aerodynamic instability and the mechanism of flutter, NACA Report No. 496, 1935.
-
(1935)
NACA Report No. 496
, vol.496
-
-
Theodorsen, T.1
-
19
-
-
0032022865
-
Experimental active control of a typical section using a trailing edge flap
-
Vipperman J.S., Clark R.L., Conner M., Dowel E.H. Experimental active control of a typical section using a trailing edge flap. J. Aircraft. 35:1998;224-229.
-
(1998)
J. Aircraft
, vol.35
, pp. 224-229
-
-
Vipperman, J.S.1
Clark, R.L.2
Conner, M.3
Dowel, E.H.4
|