-
1
-
-
0009337927
-
To MRB or not to be: Intrinsic manufacturing variabilities and effects on load carrying capacity
-
Hilton Head, SC, 1-4 November
-
McGettrick, M. and Abbott, R., To MRB or not to be: intrinsic manufacturing variabilities and effects on load carrying capacity. In Proc. 10th DoD/NASA/FAA Conf. on Fibrous Composites in Structural Design, Hilton Head, SC, 1-4 November 1993. Vol. 1. p. V-39.
-
(1993)
Proc. 10th DoD/NASA/FAA Conf. on Fibrous Composites in Structural Design
, vol.1
-
-
McGettrick, M.1
Abbott, R.2
-
2
-
-
30244446218
-
Fabrication of the V-22 composite aft fuselage using automated fiber placement
-
Seattle, WA, 29 October 1 November; NASA CP 3104
-
Pinckney, R.L., Fabrication of the V-22 composite aft fuselage using automated fiber placement. In Proc. First NASA Advanced Composites Technology Conf., Seattle, WA, 29 October 1 November 1990, pp. 385-397; NASA CP 3104.
-
(1990)
Proc. First NASA Advanced Composites Technology Conf.
, pp. 385-397
-
-
Pinckney, R.L.1
-
3
-
-
85002762095
-
Structural efficiency study of graphite-epoxy aircraft rib structures
-
Swanson, G.D., Gurdal, Z. and Starnes, J.H., Structural efficiency study of graphite-epoxy aircraft rib structures. J. Aircraft, 1990, 27, 1011-1020.
-
(1990)
J. Aircraft
, vol.27
, pp. 1011-1020
-
-
Swanson, G.D.1
Gurdal, Z.2
Starnes, J.H.3
-
4
-
-
0027148307
-
Optimum design of composite stiffened panels under combined loading
-
La Jolla, CA, 19-22 April; AIAA Paper 93-1562
-
Bushnell, D. and Bushnell, W.D., Optimum design of composite stiffened panels under combined loading. In Proc. 34th AIAA ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conf., La Jolla, CA, 19-22 April 1993, pp. 2194-2228; AIAA Paper 93-1562.
-
(1993)
Proc. 34th AIAA ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conf.
, pp. 2194-2228
-
-
Bushnell, D.1
Bushnell, W.D.2
-
5
-
-
0345028293
-
The effects of design details on cost and weight of fuselage structures
-
Long Beach, CA. June
-
Swanson, G.D., Metschan, S.L., Morris, M.R. and Kassapoglou, C., The effects of design details on cost and weight of fuselage structures. In Proc. 3rd NASA Advanced Composites Technology Conf., Long Beach, CA. June 1992, pp. 601-622.
-
(1992)
Proc. 3rd NASA Advanced Composites Technology Conf.
, pp. 601-622
-
-
Swanson, G.D.1
Metschan, S.L.2
Morris, M.R.3
Kassapoglou, C.4
-
6
-
-
0028714062
-
The use of COSTADE in developing composite commercial aircraft fuselage structures
-
Hilton Head, SC; AIAA Paper 94-1492
-
Mabson. G.E., Flynn, B.W., Ilcewicz, L.B. and Graesser, D.L., The use of COSTADE in developing composite commercial aircraft fuselage structures. In Proc. 35th AIAA/ASME/ASCE/ AHS/ASC Structures, Structural Dynamics and Materials Conf. Hilton Head, SC, 1994; AIAA Paper 94-1492.
-
(1994)
Proc. 35th AIAA/ASME/ASCE/ AHS/ASC Structures, Structural Dynamics and Materials Conf.
-
-
Mabson, G.E.1
Flynn, B.W.2
Ilcewicz, L.B.3
Graesser, D.L.4
-
7
-
-
0009341690
-
Advanced composite fuselage technology
-
Lake Tahoe, NV.
-
Olson, J.T., Smith, P.J. and Ilcewicz, L.B., Advanced composite fuselage technology. In Proc. 10th DoD/NASA/FAA Conference on Fibrous Composites in Structural Design, Lake Tahoe, NV. 1991.
-
(1991)
Proc. 10th DoD/NASA/FAA Conference on Fibrous Composites in Structural Design
-
-
Olson, J.T.1
Smith, P.J.2
Ilcewicz, L.B.3
-
8
-
-
0028732175
-
Development of a theoretical cost model for advanced composites fabrication
-
Gutowski, T., Hoult, D., Dillon, G., Neoh, E., Muter. S., Kim, E. and Tse, M., Development of a theoretical cost model for advanced composites fabrication. Compos. Manuf., 1994, 5(4), 231-239.
-
(1994)
Compos. Manuf.
, vol.5
, Issue.4
, pp. 231-239
-
-
Gutowski, T.1
Hoult, D.2
Dillon, G.3
Neoh, E.4
Muter, S.5
Kim, E.6
Tse, M.7
-
9
-
-
0003630136
-
-
S.R. Jacobs & Associates Inc., Indianapolis, IN, Section C5.11
-
Bruhn, E.F., Analysis and Design of Flight Vehicle Structures. S.R. Jacobs & Associates Inc., Indianapolis, IN, 1973, Section C5.11.
-
(1973)
Analysis and Design of Flight Vehicle Structures
-
-
Bruhn, E.F.1
-
10
-
-
0003544435
-
-
Technomic Publishing Co., Lancaster, PA, Ch. 5.7
-
Whitney, J.M., Structural Analysis of Laminated Anisotropic Plates. Technomic Publishing Co., Lancaster, PA, 1987, Ch. 5.7.
-
(1987)
Structural Analysis of Laminated Anisotropic Plates
-
-
Whitney, J.M.1
-
11
-
-
0003491390
-
-
McGraw Hill, New York, NY, Ch. 11
-
Timoshenko, S. and Woinowsky-Krieger, S., Theory of Plates and Shells. McGraw Hill, New York, NY, 1959, Ch. 11.
-
(1959)
Theory of Plates and Shells
-
-
Timoshenko, S.1
Woinowsky-Krieger, S.2
-
12
-
-
0024929584
-
Buckling and vibration of finite length composite prismatic plate structures with diaphragm ends, part II: Computer programs and buckling applications
-
Peshkam, V. and Dawe, D.J., Buckling and vibration of finite length composite prismatic plate structures with diaphragm ends, Part II: computer programs and buckling applications. Comput. Meth. Appl. Mech. Eng., 1989, 77, 227-252.
-
(1989)
Comput. Meth. Appl. Mech. Eng.
, vol.77
, pp. 227-252
-
-
Peshkam, V.1
Dawe, D.J.2
-
13
-
-
0028583340
-
The buckling performance of composite stiffened panel structures, subjected to combined in-plane compression and shear loading
-
Loughlan, J., The buckling performance of composite stiffened panel structures, subjected to combined in-plane compression and shear loading. Compos. Struct., 1994, 29, 197-212.
-
(1994)
Compos. Struct.
, vol.29
, pp. 197-212
-
-
Loughlan, J.1
-
14
-
-
0005340408
-
Mechanics of composite materials
-
Tsai, S.W., Mechanics of composite materials. AFML-TR-66-149, 1966, p. 15.
-
(1966)
AFML-TR-66-149
, pp. 15
-
-
Tsai, S.W.1
-
15
-
-
0041506589
-
The ultimate strength of aluminum alloy formed structural shapes in compression
-
Needham, R.A., The ultimate strength of aluminum alloy formed structural shapes in compression. J. Aeronaut. Sci., 1954, 21, 217-229.
-
(1954)
J. Aeronaut. Sci.
, vol.21
, pp. 217-229
-
-
Needham, R.A.1
|