-
1
-
-
0028501727
-
Static shape control for adaptive wings
-
Austin, F., M. J. Rossi, W. Van Nostrand and G. Knowles. 1994. "Static shape control for adaptive wings," AIAA Journal, 32, pp. 1895-1901.
-
(1994)
AIAA Journal
, vol.32
, pp. 1895-1901
-
-
Austin, F.1
Rossi, M.J.2
Van Nostrand, W.3
Knowles, G.4
-
2
-
-
0343258167
-
Adaptive flight control surfaces, wings, rotors and active aerodynamics
-
SPIE Paper
-
Barrett, R. and F. Brozoski. 1996. "Adaptive flight control surfaces, wings, rotors and active aerodynamics," Smart Structures and Materials 1996 Conference, SPIE Paper 2717-11.
-
(1996)
Smart Structures and Materials 1996 Conference
, pp. 2717-2811
-
-
Barrett, R.1
Brozoski, F.2
-
3
-
-
84907685991
-
Adaptive wing model for wind channel tests
-
Braunschweig, Germany, May 2000
-
Campanile, L. F., V. Carli and D. Sachau. 2000. "Adaptive wing model for wind channel tests," Active Control Technology for Enhanced Performance Operation Capabilities of Military Aircraft, Land Vehicles and Sea Vehicles, Braunschweig, Germany, May 2000.
-
(2000)
Active Control Technology for Enhanced Performance Operation Capabilities of Military Aircraft, Land Vehicles and Sea Vehicles
-
-
Campanile, L.F.1
Carli, V.2
Sachau, D.3
-
4
-
-
0343258166
-
-
US-Patent 6 010 098
-
Campanile, L. F. and H. Hanselka. 1998. "Aerodynamic structure for a landing flap, an airfoil, an elevator unit or a rudder unit, with a changeable cambering," US-Patent 6 010 098.
-
(1998)
Aerodynamic Structure for a Landing Flap, An Airfoil, An Elevator Unit or a Rudder Unit, with a Changeable Cambering
-
-
Campanile, L.F.1
Hanselka, H.2
-
6
-
-
0004923990
-
Review of current status of smart structures and integrated systems
-
SPIE Paper
-
Chopra, I. 1996. "Review of current status of smart structures and integrated systems," Smart Structures and Materials 1996 Conference, SPIE Paper 2717-01.
-
(1996)
Smart Structures and Materials 1996 Conference
, pp. 2717-2801
-
-
Chopra, I.1
-
8
-
-
84859411586
-
-
US-Patent No. 4,247,066
-
Frost, R. C., E. W. Gomez and R. W. McAnally. 1981. "Airfoil variable camber device and method," US-Patent No. 4,247,066
-
(1981)
Airfoil Variable Camber Device and Method
-
-
Frost, R.C.1
Gomez, E.W.2
McAnally, R.W.3
-
9
-
-
0025056224
-
The development and design integration of a variable camber wing for long/medium range aircraft
-
Greff, E. 1990. "The development and design integration of a variable camber wing for long/medium range aircraft," AIAA Journal, 94, pp. 301-312
-
(1990)
AIAA Journal
, vol.94
, pp. 301-312
-
-
Greff, E.1
-
11
-
-
0021696362
-
Variable wing camber control for civil transport aircraft
-
ICAS-Paper No. 84-5.2.1.
-
Hilbig, H. and H. Wagner, 1984. "Variable wing camber control for civil transport aircraft," ICAS-84 Conference, ICAS-Paper No. 84-5.2.1.
-
(1984)
ICAS-84 Conference
-
-
Hilbig, H.1
Wagner, H.2
-
12
-
-
0004849459
-
Active vibration suppression systems applied to twin tail buffeting
-
SPIE Paper 3326-05
-
Hopkins, M., D. Henderson, R. Moses, T. Ryall, D. Zimcik, R. Spangler. 1998. "Active vibration suppression systems applied to twin tail buffeting," Smart Structures and Materials 1998 Conference, SPIE Paper 3326-05.
-
(1998)
Smart Structures and Materials 1998 Conference
-
-
Hopkins, M.1
Henderson, D.2
Moses, R.3
Ryall, T.4
Zimcik, D.5
Spangler, R.6
-
18
-
-
84915226631
-
Mission adaptive wing camber control systems for transport aircraft
-
AIAA-Paper 85-5006
-
Renken, J. H. 1985. "Mission adaptive wing camber control systems for transport aircraft," AIAA 3rd Applied Aerodynamics Conference, AIAA-Paper 85-5006.
-
(1985)
AIAA 3rd Applied Aerodynamics Conference
-
-
Renken, J.H.1
-
21
-
-
0026617486
-
The use of variable camber to reduce drag, weight and costs of transport aircraft
-
Spillman, J. J. 1992. "The use of variable camber to reduce drag, weight and costs of transport aircraft," Aeronautical Journal 96, pp. 1-9.
-
(1992)
Aeronautical Journal
, vol.96
, pp. 1-9
-
-
Spillman, J.J.1
-
22
-
-
0342823356
-
-
US-Patent No. 4,351,502, 1982
-
Statkus, F. D. 1982. "Continuous skin, variable camber airfoil edge actuating mechanism," US-Patent No. 4,351,502, 1982
-
(1982)
Continuous Skin, Variable Camber Airfoil Edge Actuating Mechanism
-
-
Statkus, F.D.1
-
23
-
-
0021828286
-
The influence of camber variation on the aerodynamics of civil transport aircraft
-
AIAA-Paper No. 85-0353
-
Szodruch, J. 1985. "The influence of camber variation on the aerodynamics of civil transport aircraft," AIAA 23rd Aerospace Sciences Meeting, AIAA-Paper No. 85-0353.
-
(1985)
AIAA 23rd Aerospace Sciences Meeting
-
-
Szodruch, J.1
|