-
1
-
-
0029380374
-
Free vibration analysis of anisotropic thin-walled closed-cross-section beams
-
Armanios E.A., and Badir A.M. Free vibration analysis of anisotropic thin-walled closed-cross-section beams. AIAA Journal 33 (1995) 1905-1910
-
(1995)
AIAA Journal
, vol.33
, pp. 1905-1910
-
-
Armanios, E.A.1
Badir, A.M.2
-
2
-
-
0027110269
-
Coupled bending-torsional dynamic stiffness matrix for Timoshenko beam elements
-
Banerjee J.R., and Williams F.W. Coupled bending-torsional dynamic stiffness matrix for Timoshenko beam elements. Computers & Structures 42 (1992) 301-310
-
(1992)
Computers & Structures
, vol.42
, pp. 301-310
-
-
Banerjee, J.R.1
Williams, F.W.2
-
3
-
-
0001224924
-
Free vibration of composite beams - an exact method using symbolic computation
-
Banerjee J.R., and Williams F.W. Free vibration of composite beams - an exact method using symbolic computation. Journal of Aircraft 32 (1995) 636-642
-
(1995)
Journal of Aircraft
, vol.32
, pp. 636-642
-
-
Banerjee, J.R.1
Williams, F.W.2
-
5
-
-
85088759910
-
-
T.M. Clements, M. Rais-Rohani, Design optimization of a composite tilt-rotor wing with stability approximations, in: Proc. of 41st AIAA/SME/ASEC/AHS/ASC Structures, Structural Dynamics and Materials Conference, Atlanta, GA, April 2000, pp. 829-838. Paper No. AIAA-2000-1454
-
-
-
-
6
-
-
34249310041
-
-
D.E. Davies, Theoretical determination of subsonic oscillatory airforce coefficients, Royal Aircraft Establishment - Technical Report (RAE-TR-76059), 1978
-
-
-
-
7
-
-
34249288790
-
-
M.A. El-Shinnawey, Ground resonance and normal modes of aerobatic aircraft Cranfield A1, MSc Experimental Thesis, College of Aeronautics, Cranfield University, December 1978
-
-
-
-
8
-
-
0000387235
-
A rapidly convergent method for minimization
-
Fletcher R., and Powell M.J.D. A rapidly convergent method for minimization. Computer Journal 6 (1963) 163-168
-
(1963)
Computer Journal
, vol.6
, pp. 163-168
-
-
Fletcher, R.1
Powell, M.J.D.2
-
11
-
-
0041762027
-
The effect of laminate lay-up on the flutter speed of composite wings
-
Guo S., Banerjee J.R., and Cheung C.W. The effect of laminate lay-up on the flutter speed of composite wings. Proc. of IMechE, Part G, J. of Aerospace Eng. 217 (2003) 115-122
-
(2003)
Proc. of IMechE, Part G, J. of Aerospace Eng.
, vol.217
, pp. 115-122
-
-
Guo, S.1
Banerjee, J.R.2
Cheung, C.W.3
-
12
-
-
28844459466
-
-
S. Guo, W. Chen, D. Cui, Optimization of composite wing structures for maximum flutter speed, in: Proc. of the 1st AIAA Multidisciplinary Design Optimization Specialist Conference, the 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Austin, TX, 18-21 April 2005. Paper No. AIAA-2005-2132
-
-
-
-
13
-
-
34249310391
-
-
S. Guo, C.W. Cheung, J.R. Banerjee, R. Butler, Gust alleviation and flutter suppression of an optimized composite wing, in: Proc. of Int. Forum on Aeroelasticity and Structural Dynamics, Manchester, UK, June 1995, pp. 41.1-41.9
-
-
-
-
15
-
-
0021197871
-
Aeroelastic flutter and divergence of stiffness coupled graphite/epoxy cantilevered plates
-
Hollowell S.J., and Dugundji J. Aeroelastic flutter and divergence of stiffness coupled graphite/epoxy cantilevered plates. Journal of Aircraft 21 (1984) 69-76
-
(1984)
Journal of Aircraft
, vol.21
, pp. 69-76
-
-
Hollowell, S.J.1
Dugundji, J.2
-
18
-
-
0024104193
-
Aeroelastic divergence of swept-forward composite wings including warping restraint effect
-
Librescu L., and Khdeir A.A. Aeroelastic divergence of swept-forward composite wings including warping restraint effect. AIAA Journal 26 (1988) 1373-1377
-
(1988)
AIAA Journal
, vol.26
, pp. 1373-1377
-
-
Librescu, L.1
Khdeir, A.A.2
-
19
-
-
0023985604
-
General formulation for the aeroelastic divergence of composite swept-forward wing structures
-
Librescu L., and Simovich J. General formulation for the aeroelastic divergence of composite swept-forward wing structures. Journal of Aircraft 25 (1988) 364-371
-
(1988)
Journal of Aircraft
, vol.25
, pp. 364-371
-
-
Librescu, L.1
Simovich, J.2
-
20
-
-
0026103397
-
Analytical study on static aeroelastic behavior of swept-forward composite wing structures
-
Librescu L., and Thangjitham S. Analytical study on static aeroelastic behavior of swept-forward composite wing structures. Journal of Aircraft 28 (1991) 151-157
-
(1991)
Journal of Aircraft
, vol.28
, pp. 151-157
-
-
Librescu, L.1
Thangjitham, S.2
-
21
-
-
0029213891
-
-
M. Lillico, R. Butler, J.R. Banerjee, S. Guo, Optimum design of high aspect ratio wings subject to aeroelastic constraints, in: Proc. of 36th AIAA/SME/ASEC/AHS/ASC Structures, Structural Dynamics and Materials Conference, April 1995, pp. 558-566
-
-
-
-
22
-
-
0031061903
-
Aeroelastic optimization of composite wings using the dynamic stiffness method
-
Lillico M., Butler R., Guo S., and Banerjee J.R. Aeroelastic optimization of composite wings using the dynamic stiffness method. The Aeronautical Journal 101 (1997) 77-86
-
(1997)
The Aeronautical Journal
, vol.101
, pp. 77-86
-
-
Lillico, M.1
Butler, R.2
Guo, S.3
Banerjee, J.R.4
-
23
-
-
0022161218
-
Flutter and divergence aeroelastic characteristics for composite forward swept cantilever wing
-
Lottati I. Flutter and divergence aeroelastic characteristics for composite forward swept cantilever wing. Journal of Aircraft 22 (1985) 1001-1007
-
(1985)
Journal of Aircraft
, vol.22
, pp. 1001-1007
-
-
Lottati, I.1
-
25
-
-
0019025136
-
Divergence of swept-forward composite wings
-
Weisshaar T.A. Divergence of swept-forward composite wings. Journal of Aircraft 17 (1980) 442-448
-
(1980)
Journal of Aircraft
, vol.17
, pp. 442-448
-
-
Weisshaar, T.A.1
|