-
1
-
-
0003566155
-
-
Noorhoff International, Leyden, The Netherlands
-
Librescu, L., Elastostatics and Kinetics of Anisotropic and Heterogeneous Sheel-Type Structures, Noorhoff International, Leyden, The Netherlands, 1975, pp. 1-281.
-
(1975)
Elastostatics and Kinetics of Anisotropic and Heterogeneous Sheel-Type Structures
, pp. 1-281
-
-
Librescu, L.1
-
2
-
-
0019899616
-
4'On the Track of Practical Forward-Swept Wings,"
-
Hertz, T. J., Shirk, M. H., Ricketts, R. H., and Weisshaar, T. A., 4'On the Track of Practical Forward-Swept Wings," Astronautics and Aeronautics, Vol. 20, Jan. 1982, pp. 40-52.
-
(1982)
Astronautics and Aeronautics
, vol.20
, pp. 40-52
-
-
Hertz, T.J.1
Shirk, M.H.2
Ricketts, R.H.3
Weisshaar, T.A.4
-
3
-
-
0022321911
-
-
Aachen, FRG, April
-
Weisshaar, T. A., "Tailoring for Aeroelastic Stability and Lateral Control Enhancement," Second International Symposium on Aeroelasticity and Structural Dynamics, DGLR-Bericht 85-02, Aachen, FRG, April 1985, pp. 415-425.
-
(1985)
Tailoring for Aeroelastic Stability and Lateral Control Enhancement," Second International Symposium on Aeroelasticity and Structural Dynamics, Dglr-Bericht 85-02
, pp. 415-425
-
-
Weisshaar, T.A.1
-
4
-
-
0022544782
-
Aeroelastic Tailoring-Theory, Practice and Promise
-
1
-
Shirk, M. H., Hertz, T. J., and Weisshaar, T. A., "Aeroelastic Tailoring-Theory, Practice and Promise," Journal of Aircraft, Vol. 23, No. 1, 1986, pp. 6-18.
-
(1986)
Journal of Aircraft
, vol.23
, pp. 6-18
-
-
Shirk, M.H.1
Hertz, T.J.2
Weisshaar, T.A.3
-
6
-
-
0019319646
-
Frequency Determination and Non-Dimensionalization for Composite Cantilever Plates
-
1
-
Crawley, E.F., and Dugundji, J., "Frequency Determination and Non-Dimensionalization for Composite Cantilever Plates," Journal of Sound and Vibration, Vol. 72, No. 1, 1980, pp. 1-10.
-
(1980)
Journal of Sound and Vibration
, vol.72
, pp. 1-10
-
-
Crawley, E.F.1
Dugundji, J.2
-
7
-
-
0020152304
-
"Vibration of Cantilevered Graphite/Epoxy Plates with Bending-Torsion Coupling
-
Jensen, D. W., Crawley, E. F., and Dugundji, J., "Vibration of Cantilevered Graphite/Epoxy Plates with Bending-Torsion Coupling, Journal of Reinforced Plastics and Composites," Vol. 1, July 1982, pp. 254-269.
-
(1982)
Journal of Reinforced Plastics and Composites,"
, vol.1
, pp. 254-269
-
-
Jensen, D.W.1
Crawley, E.F.2
Dugundji, J.3
-
8
-
-
0023164420
-
Composite Box Beam Analysis: Theory and Experiments
-
Bauchau, O. A., Coffenberry, B. S., and Rehfield, L. W., "Composite Box Beam Analysis: Theory and Experiments," Journal of Reinforced Plastics and Composites, Vol. 6, Jan. 1987, pp. 25-34.
-
(1987)
Journal of Reinforced Plastics and Composites
, vol.6
, pp. 25-34
-
-
Bauchau, O.A.1
Coffenberry, B.S.2
Rehfield, L.W.3
-
9
-
-
84909835055
-
Some Considerations on the Nonclassical Behavior of Thin-Walled Composite Beams
-
Williamsburg, VA, Oct
-
Rehfield, L. W., Hodges, D. H., and Atilgan, A. R., "Some Considerations on the Nonclassical Behavior of Thin-Walled Composite Beams," presented at the American Helicopter Society National Technical Specialists' Meeting on Advanced Rotocraft Structures, Williamsburg, VA, Oct. 1988.
-
(1988)
Presented at the American Helicopter Society National Technical Specialists' Meeting on Advanced Rotocraft Structures
-
-
Rehfield, L.W.1
Hodges, D.H.2
Atilgan, A.R.3
-
10
-
-
0024608933
-
Some Implications of Warping Restraint on the Behavior of Composite Anisotropic Beams
-
2
-
Oybo, G. A., "Some Implications of Warping Restraint on the Behavior of Composite Anisotropic Beams," Journal Aircraft, Vol. 26, No. 2, 1989, pp. 187-189.
-
(1989)
Journal Aircraft
, vol.26
, pp. 187-189
-
-
Oybo, G.A.1
-
11
-
-
0022161218
-
Flutter and Divergence Aeroelastic Characteristics for Composite Forward Swept Cantilevered Wing
-
11
-
Lottati, I., "Flutter and Divergence Aeroelastic Characteristics for Composite Forward Swept Cantilevered Wing," Journal Aircraft, Vol. 22, No. 11, 1985, pp. 1001-1007.
-
(1985)
Journal Aircraft
, vol.22
, pp. 1001-1007
-
-
Lottati, I.1
-
12
-
-
0023985604
-
A General Formulation for the Aeroelastic Divergence of Composite Swept Forward Wing Structures
-
4
-
Librescu, L., and Simovich, J., "A General Formulation for the Aeroelastic Divergence of Composite Swept Forward Wing Structures," Journal of Aircraft, Vol. 25, No. 4, 1988, pp. 364-371.
-
(1988)
Journal of Aircraft
, vol.25
, pp. 364-371
-
-
Librescu, L.1
Simovich, J.2
-
13
-
-
0024104193
-
Aeroelastic Divergence of Sweptforward Composite Wings Including Warping Restraint Effect
-
11
-
Librescu, L., and Khdeir, A. A., "Aeroelastic Divergence of Sweptforward Composite Wings Including Warping Restraint Effect," AIAA Journal, Vol. 26, No. 11, 1988, pp. 1373-1377.
-
(1988)
AIAA Journal
, vol.26
, pp. 1373-1377
-
-
Librescu, L.1
Khdeir, A.A.2
-
14
-
-
85002922511
-
-
AIAA Paper 88-2209, April
-
Librescu, L., and Thangjitham, S., "The Influence of the Warping Restraint on the Spanwise Lift Distribution of Swept Forward Composite Wing Structures," AIAA Paper 88-2209, April 1988.
-
(1988)
The Influence of the Warping Restraint on the Spanwise Lift Distribution of Swept Forward Composite Wing Structures,"
-
-
Librescu, L.1
Thangjitham, S.2
-
15
-
-
84909844585
-
The Static Aeroelastic Behavior of Sweptforward Composite Wing Structures Taking into Account Their Warping Restraint Effect
-
Technomic
-
Librescu, L., and Thangjitham, S., "The Static Aeroelastic Behavior of Sweptforward Composite Wing Structures Taking into Account Their Warping Restraint Effect," Proceedings of the Fourth Japan-U.S. Conference on Composite Materials, Technomic, 1988, pp. 914-922.
-
(1988)
Proceedings of the Fourth Japan-U.S. Conference on Composite Materials
, pp. 914-922
-
-
Librescu, L.1
Thangjitham, S.2
-
16
-
-
85072412404
-
The Warping Restraint Effect in the Critical and Subcritical Static Aeroelastic Behavior of Swept Forward Composite Wing Structures
-
Paper 891056April
-
Librescu, L., and Thangjitham, S., "The Warping Restraint Effect in the Critical and Subcritical Static Aeroelastic Behavior of Swept Forward Composite Wing Structures," Society of Automotive Engineers, Paper 891056, April 1989.
-
(1989)
Society of Automotive Engineers
-
-
Librescu, L.1
Thangjitham, S.2
-
17
-
-
85003253953
-
Aeroelastic Divergence of Multicell Wings Taking Their Fixing Restraints into Account
-
6
-
Petre, A., Stanescu, C., and Librescu, L., "Aeroelastic Divergence of Multicell Wings Taking Their Fixing Restraints into Account," Revue de Mecanique Appliquee, Vol. 19, No. 6, 1961, pp. 689-698.
-
(1961)
Revue De Mecanique Appliquee
, vol.19
, pp. 689-698
-
-
Petre, A.1
Stanescu, C.2
Librescu, L.3
-
18
-
-
56949084527
-
-
Edit. Academiei Republicii Socialiste Romania, Bucarest
-
Petre, A., Teoria Aeroelasticitatii, Statiaca, Edit. Academiei Republicii Socialiste Romania, Bucarest, 1966.
-
(1966)
Teoria Aeroelasticitatii, Statiaca
-
-
Petre, A.1
-
20
-
-
85002644019
-
Forward Swept Wings: Static Aeroelasticity
-
AFFDL-TR-3087, June
-
Weisshaar, T. A., "Forward Swept Wings: Static Aeroelasticity," Air Force Dynamics Laboratory, AFFDL-TR-3087, June 1979.
-
(1979)
Air Force Dynamics Laboratory
-
-
Weisshaar, T.A.1
-
21
-
-
0019025136
-
Divergence of Forward Swept Composite Wings
-
6
-
Weisshaar, T. A., "Divergence of Forward Swept Composite Wings," Journal of Aircraft, Vol. 17, No. 6, 1980, pp. 442-448.
-
(1980)
Journal of Aircraft
, vol.17
, pp. 442-448
-
-
Weisshaar, T.A.1
-
22
-
-
85003347198
-
Aeroelastic Divergence of Unrestrained Vehicles
-
12
-
Rodden, W. P., "Aeroelastic Divergence of Unrestrained Vehicles," Journal of Aircraft, Vol. 18, No. 12, 1981, pp. 1072-1073.
-
(1981)
Journal of Aircraft
, vol.18
, pp. 1072-1073
-
-
Rodden, W.P.1
-
23
-
-
85003273943
-
Aeroelastic Divergence of Unrestrained Vehicles
-
1
-
Rodden, W. P., "Aeroelastic Divergence of Unrestrained Vehicles," Journal of Aircraft, Vol. 21, No. 1, 1984, pp. 94-96.
-
(1984)
Journal of Aircraft
, vol.21
, pp. 94-96
-
-
Rodden, W.P.1
-
24
-
-
85003346463
-
Unrestrained Aeroelastic Divergence in a Dynamic Stability Analysis
-
9
-
Rodden, W. P., and Bellinger, E. D., "Unrestrained Aeroelastic Divergence in a Dynamic Stability Analysis," Journal of Aircraft, Vol. 19, No. 9, 1982, pp. 796-797.
-
(1982)
Journal of Aircraft
, vol.19
, pp. 796-797
-
-
Rodden, W.P.1
Bellinger, E.D.2
-
25
-
-
0021392562
-
Active Suppression of Aeroelastic Instabilities on a Forward-Swept Wing
-
3
-
Noll, T. L., Eastep, F. E., and Calico, R. A., "Active Suppression of Aeroelastic Instabilities on a Forward-Swept Wing," Journal of Aircraft, Vol. 21, No. 3, 1984, pp. 202-208.
-
(1984)
Journal of Aircraft
, vol.21
, pp. 202-208
-
-
Noll, T.L.1
Eastep, F.E.2
Calico, R.A.3
-
26
-
-
85002685478
-
Experimental Studies in Aeroelasticity of Unswept and Forward Swept Graphite/Epoxy Wings
-
edited by P. Hajela, Univ. Press of Florida, Gainesville, FL
-
Dugundji, J., "Experimental Studies in Aeroelasticity of Unswept and Forward Swept Graphite/Epoxy Wings," Recent Trends in Aeroelasticity, Structures and Structural Design, edited by P. Hajela, Univ. Press of Florida, Gainesville, FL, 1987, pp. 149-160.
-
(1987)
Recent Trends in Aeroelasticity, Structures and Structural Design
, pp. 149-160
-
-
Dugundji, J.1
-
27
-
-
0023385792
-
Experimental Aeroelastic Behavior of Forward-Swept Graphite/Epoxy Wings with Rigid-Body Freedom
-
7
-
Chen, G. S., and Dugundji, J., "Experimental Aeroelastic Behavior of Forward-Swept Graphite/Epoxy Wings with Rigid-Body Freedom," Journal of Aircraft, Vol. 24, No. 7, 1987, pp. 454-462.
-
(1987)
Journal of Aircraft
, vol.24
, pp. 454-462
-
-
Chen, G.S.1
Dugundji, J.2
-
28
-
-
84909871939
-
-
Massachusetts Inst. of Techology, Cambridge, MA, TELAC Rept. 86-14, May
-
Chen, G. S., and Dugundji, J., "Aeroelastic Behavior of Forward Swept Graphite/Epoxy Wing Aircraft with Rigid Body Freedoms," Massachusetts Inst. of Techology, Cambridge, MA, TELAC Rept. 86-14, May 1986.
-
(1986)
Aeroelastic Behavior of Forward Swept Graphite/Epoxy Wing Aircraft with Rigid Body Freedoms,"
-
-
Chen, G.S.1
Dugundji, J.2
-
29
-
-
0022785468
-
Aeroelastic Divergence of Trimmed Aircraft
-
9
-
Niblett, L. T., "Aeroelastic Divergence of Trimmed Aircraft," Journal of Aircraft, Vol. 23, No. 9, 1986, pp. 727-729.
-
(1986)
Journal of Aircraft
, vol.23
, pp. 727-729
-
-
Niblett, L.T.1
-
30
-
-
0023450732
-
Aeroelastic Stability Characteristics of a Composite Swept Wing with Tip Weights for an Unrestrained Vehicle
-
11
-
Lottati, I., "Aeroelastic Stability Characteristics of a Composite Swept Wing with Tip Weights for an Unrestrained Vehicle," Journal of Aircraft, Vol. 24, No. 11, 1987, pp. 793-802.
-
(1987)
Journal of Aircraft
, vol.24
, pp. 793-802
-
-
Lottati, I.1
-
32
-
-
0021119797
-
Generic Approach to Determine Optimum Aeroelastic Characteristics for Composite Forward-Swept-Wing Aircraft
-
1
-
Oyibo, G. A., "Generic Approach to Determine Optimum Aeroelastic Characteristics for Composite Forward-Swept-Wing Aircraft," AIAA Journal, Vol. 22, No. 1, 1984, pp. 117-123.
-
(1984)
AIAA Journal
, vol.22
, pp. 117-123
-
-
Oyibo, G.A.1
-
33
-
-
84966677230
-
-
Adison-Wesley, Reading, MA
-
Bisplinghoff, R. L., Ashley, H., and Halfman, R. L., Aeroelasticity, Adison-Wesley, Reading, MA, 1955.
-
(1955)
Aeroelasticity
-
-
Bisplinghoff, R.L.1
Ashley, H.2
Halfman, R.L.3
-
34
-
-
0004888460
-
-
Ph.D. Dissertation, Stanford Univ., Stanford, CA, Feb, NASA CR Rept. 3591
-
Lehman, L. L., "Hybrid State Vector Methods for Structural Dynamics and Aeroelastic Boundary Value Problems," Ph.D. Dissertation, Stanford Univ., Stanford, CA, Feb. 1982, also NASA CR Rept. 3591.
-
(1982)
Hybrid State Vector Methods for Structural Dynamics and Aeroelastic Boundary Value Problems,"
-
-
Lehman, L.L.1
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