-
1
-
-
79957564185
-
Typical Section Model of an Airfoil
-
2nd Edition, Kluwer Academic Publishers
-
Dowell, E. H. (editor), Curtiss, H. C. Jr., Scanlan, R. H., and Sisto, F., 'Typical Section Model of an Airfoil," A Modern Course in Aeroelasticitv. 2nd Edition, Kluwer Academic Publishers, 1989, pp. 12, 267
-
(1989)
A Modern Course in Aeroelasticitv
-
-
Dowell, E.H.1
Curtiss, H.C.2
Scanlan, R.H.3
Sisto, F.4
-
2
-
-
0025211734
-
Nonlinear Aeroelasticity
-
American Institute of Aeronautics and Astronautics, AIAA Paper No. 90-1031
-
Dowell, E. H., "Nonlinear Aeroelasticity," Proceedings of the AIAA 31st Structures. Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, AIAA Paper No. 90-1031, 1990, pp. 1497-1509.
-
(1990)
Proceedings of the AIAA 31st Structures. Structural Dynamics, and Materials Conference
, pp. 1497-1509
-
-
Dowell, E.H.1
-
3
-
-
0025252943
-
Effects of Spoiler Surfaces on the Aeroelastic Behavior of a Low-Aspect Ratio Wing
-
American Institute of Aeronautics and Astronautics, AIAA paper 90-0981, April
-
Cole, S. R., "Effects of Spoiler Surfaces on the Aeroelastic Behavior of a Low-Aspect Ratio Wing," Proceedings of the 31st AIAA Structures. Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, AIAA paper 90-0981, April 1990, pp. 1455-1463.
-
(1990)
Proceedings of the 31st AIAA Structures. Structural Dynamics, and Materials Conference
, pp. 1455-1463
-
-
Cole, S.R.1
-
4
-
-
0001935145
-
An Investigation of Effects of Certain Types of Structural Nonlinearities on Wing and Control Surface Flutter
-
WooIston, Donald S., Runyan, Harry L., Andrews, Robert E., "An Investigation of Effects of Certain Types of Structural Nonlinearities on Wing and Control Surface Flutter," J. Aero. ScL Vol. 24, No. 1, Jan. 1957, pp. 57-63.
-
(1957)
J. Aero. ScL
, vol.24
, Issue.1
, pp. 57-63
-
-
WooIston, D.S.1
Runyan, H.L.2
Andrews, R.E.3
-
5
-
-
0004090934
-
-
NASA technical paper 1620, March, National Aeronautics and Space Administration, Hampton, Virginia
-
Breitbach, Elmar J., "Flutter Analysis of an Airplane with Multiple Structural Nonlinearities in the Control System," NASA technical paper 1620, March 1980, National Aeronautics and Space Administration, Hampton, Virginia.
-
(1980)
Flutter Analysis of an Airplane with Multiple Structural Nonlinearities in the Control System
-
-
Breitbach, E.J.1
-
6
-
-
0004252591
-
-
AGARD-R-665, Jan., North Atlantic Treaty Organization, Neuilly sur Seine, France
-
Breitbach, E., "Effects of Structural Nonlinearities on Aircraft Vibration and Flutter," AGARD-R-665, Jan. 1978, North Atlantic Treaty Organization, Neuilly sur Seine, France.
-
(1978)
Effects of Structural Nonlinearities on Aircraft Vibration and Flutter
-
-
Breitbach, E.1
-
7
-
-
84962182141
-
-
Science and Technology of Low Speed and Motorless Flight. National Aeronautics and Space Administration, NASA CP-2085, Part II
-
Breitbach, Elmar J., "Treatment of the Control Mechanism of Light Airplanes in the Flutter Clearance Process," Science and Technology of Low Speed and Motorless Flight. National Aeronautics and Space Administration, NASA CP-2085, Part II, 1979, pp. 437-466.
-
(1979)
Treatment of the Control Mechanism of Light Airplanes in the Flutter Clearance Process
, pp. 437-466
-
-
Breitbach, E.J.1
-
8
-
-
0343736765
-
-
NASA TM 83302, April, National Aeronautics and Space Administration, Hampton Virginia
-
Farmer, M., "A Two Degree of Freedom Flutter Mount System with Low Damping for Testing Rigid Wings at Different Angles of Attack," NASA TM 83302, April 1982, National Aeronautics and Space Administration, Hampton Virginia.
-
(1982)
A Two Degree of Freedom Flutter Mount System with Low Damping for Testing Rigid Wings at Different Angles of Attack
-
-
Farmer, M.1
-
9
-
-
0142049250
-
-
NASA TM 107581,, National Aeronautics and Space Administration, Hampton Virginia
-
Rivera, Jose A. Jr, Dansbury, Bryan E., Bennett, Robert M., Durham, Michael H., Silva, Walter A., "NACA 0012 Benchmark Model Experimental Flutter Results with Unsteady Pressure Distributions," NASA TM 107581, 1992, National Aeronautics and Space Administration, Hampton Virginia.
-
(1992)
NACA 0012 Benchmark Model Experimental Flutter Results with Unsteady Pressure Distributions
-
-
Rivera, J.A.1
Dansbury, B.E.2
Bennett, R.M.3
Durham, M.H.4
Silva, W.A.5
-
10
-
-
0005278076
-
-
National Aeronautical Establishment-Aeronautical Note-36, National Research Council (Canada) No. 25438, Ottawa, Quebec, Canada, February
-
Lee, B. H. K. and LeBianc, P., "Flutter Analysis of a Two-dimensional Airfoil with Cubic Nonlinear Restoring Force," National Aeronautical Establishment-Aeronautical Note-36, National Research Council (Canada) No. 25438, Ottawa, Quebec, Canada, February, 1986.
-
(1986)
Flutter Analysis of a Two-dimensional Airfoil with Cubic Nonlinear Restoring Force
-
-
Lee, B.H.K.1
LeBianc, P.2
-
11
-
-
84962181547
-
-
National Aeronautical Establishment-Aeronautical Report LR-618, National Research Council (Canada) No. 27833, Ottawa, Quebec, Canada, May
-
Lee, B. H. K., and Desrochers, J., "Flutter Analysis of a Two-Dimensional Airfoil Containing Structural Nonlinearities," National Aeronautical Establishment-Aeronautical Report LR-618, National Research Council (Canada) No. 27833, Ottawa, Quebec, Canada, May, 1987.
-
(1987)
Flutter Analysis of a Two-Dimensional Airfoil Containing Structural Nonlinearities
-
-
Lee, B.H.K.1
Desrochers, J.2
-
12
-
-
0025213824
-
Chaotic Response of Aerosurfaces with Structural Nonlinearities
-
American Institute of Aeronautics and Astronautics, AIAA Paper 90-1034
-
Hauenstein, J., Laurenson, R. M., Eversman, W., Galecki, G., Qumei, I., and Amos, A. K., "Chaotic Response of Aerosurfaces with Structural Nonlinearities," Proceedings of the 31st AIAA Structures. Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, AIAA Paper 90-1034, 1990, pp. 1530-1539.
-
(1990)
Proceedings of the 31st AIAA Structures. Structural Dynamics, and Materials Conference
, pp. 1530-1539
-
-
Hauenstein, J.1
Laurenson, R.M.2
Eversman, W.3
Galecki, G.4
Qumei, I.5
Amos, A.K.6
-
13
-
-
0028712962
-
The Aeroelastic Response of a TwoDimensional Airfoil with Bilinear and Cubic Structural Nonlinearities
-
American Institute of Aeronautics and Astronautics, AIAA Paper 94-1546
-
Price, S. J., Alighanbari, H., and Lee, B. H. K., "The Aeroelastic Response of a TwoDimensional Airfoil with Bilinear and Cubic Structural Nonlinearities," Proceedings of the 35th AIAA Structures. Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, AIAA Paper 94-1546, 1994, pp. 1771-1780.
-
(1994)
Proceedings of the 35th AIAA Structures. Structural Dynamics, and Materials Conference
, pp. 1771-1780
-
-
Price, S.J.1
Alighanbari, H.2
Lee, B.H.K.3
-
14
-
-
0028546375
-
Postinstability Behavior of a Two-Dimensional Airfoil with a Structural Nonlinearity
-
November-December
-
Price, S. J., Alighanbari, H., and Lee, B. H. K., "Postinstability Behavior of a Two-Dimensional Airfoil with a Structural Nonlinearity," Journal of Aircraft. Vol. 31. No. 6, November-December 1994, pp. 1395-1401.
-
(1994)
Journal of Aircraft
, vol.31
, Issue.6
, pp. 1395-1401
-
-
Price, S.J.1
Alighanbari, H.2
Lee, B.H.K.3
-
15
-
-
0003927402
-
-
NACA Report 496,, National Advisory Committee for Aeronautics, Hampton, Virginia
-
Theodorsen, T" "General Theory of Aerodynamic Instability and the Mechanism of Flutter," NACA Report 496, 1935, National Advisory Committee for Aeronautics, Hampton, Virginia.
-
(1935)
General Theory of Aerodynamic Instability and the Mechanism of Flutter
-
-
Theodorsen, T.1
-
16
-
-
2342470536
-
An Elementary Explanation of the Flutter Mechanism
-
Institute of the Aeronautical Sciences, Ft. Worth, TX, Nov
-
Pines, S., "An Elementary Explanation of the Flutter Mechanism," Proceedings of the National Specialists Meeting ByoMates and Aeroelasticitv. Institute of the Aeronautical Sciences, Ft. Worth, TX, Nov. 1958, pp. 52-58.
-
(1958)
Proceedings of the National Specialists Meeting ByoMates and Aeroelasticitv
, pp. 52-58
-
-
Pines, S.1
|