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Results:
1-11
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Results: 11
Authors:
JAUNKY N
KNIGHT NF
AMBUR DR
Citation: N. Jaunky et al., OPTIMAL-DESIGN OF GENERAL STIFFENED COMPOSITE CIRCULAR-CYLINDERS FOR GLOBAL BUCKLING WITH STRENGTH CONSTRAINTS, Composite structures, 41(3-4), 1998, pp. 243-252
Authors:
JAUNKY N
KNIGHT NF
AMBUR DR
Citation: N. Jaunky et al., OPTIMAL-DESIGN OF GRID-STIFFENED COMPOSITE PANELS USING GLOBAL AND LOCAL BUCKLING ANALYSES, Journal of aircraft, 35(3), 1998, pp. 478-486
Authors:
JAUNKY N
KNIGHT NF
AMBUR DR
Citation: N. Jaunky et al., FORMULATION OF AN IMPROVED SMEARED STIFFENER THEORY FOR BUCKLING ANALYSIS OF GRID-STIFFENED COMPOSITE PANELS, Composites. Part B, Engineering, 27(5), 1996, pp. 519-526
Authors:
ROUSE M
AMBUR DR
Citation: M. Rouse et Dr. Ambur, DAMAGE TOLERANCE AND FAILURE ANALYSIS OF A COMPOSITE GEODESICALLY STIFFENED COMPRESSION PANEL, Journal of aircraft, 33(3), 1996, pp. 582-588
Authors:
AMBUR DR
CERRO JA
DICKSON J
Citation: Dr. Ambur et al., D-BOX FIXTURE FOR TESTING STIFFENED PANELS IN COMPRESSION AND PRESSURE, Journal of aircraft, 32(6), 1995, pp. 1382-1389
Authors:
AMBUR DR
PRASAD CB
WATERS WA
Citation: Dr. Ambur et al., A DROPPED-WEIGHT APPARATUS FOR LOW-SPEED IMPACT TESTING OF COMPOSITE STRUCTURES, Experimental mechanics, 35(1), 1995, pp. 77-82
Authors:
JAUNKY N
KNIGHT NF
AMBUR DR
Citation: N. Jaunky et al., BUCKLING OF ARBITRARY QUADRILATERAL ANISOTROPIC PLATES, AIAA journal, 33(5), 1995, pp. 938-944
Authors:
AMBUR DR
STARNES JH
Citation: Dr. Ambur et Jh. Starnes, LOW-SPEED IMPACT DAMAGE-INITIATION CHARACTERISTICS OF SELECTED LAMINATED COMPOSITE PLATES, AIAA journal, 33(10), 1995, pp. 1919-1925
Authors:
REHFIELD LW
ZISCHKA PJ
CHANG S
FENTRESS ML
AMBUR DR
Citation: Lw. Rehfield et al., EXPERIMENTAL EVALUATION OF A BOX BEAM SPECIFICALLY TAILORED FOR CHORDWISE DEFORMATION, AIAA journal, 33(1), 1995, pp. 116-119
Authors:
PRASAD CB
AMBUR DR
STARNES JH
Citation: Cb. Prasad et al., RESPONSE OF LAMINATED COMPOSITE PLATES TO LOW-SPEED IMPACT BY DIFFERENT IMPACTORS, AIAA journal, 32(6), 1994, pp. 1270-1277
Authors:
AMBUR DR
REHFIELD LW
Citation: Dr. Ambur et Lw. Rehfield, EFFECT OF STIFFNESS CHARACTERISTICS ON THE RESPONSE OF COMPOSITE GRID-STIFFENED STRUCTURES, Journal of aircraft, 30(4), 1993, pp. 541-546
Risultati:
1-11
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