Stiffness design method of symmetric laminates using lamination parameters
作者： Hisao Fukunaga , Hideki Sekine
DOI: 10.2514/3.11304
关键词: Stiffness 、 Structural engineering 、 Heat generation 、 Combustion 、 Lamination (topology) 、 Structural mechanics 、 Aeroelasticity 、 Composite number 、 Materials science 、 Composite material 、 Propellant
摘要: Hermance, C. E., "A Model of Composite Propellant Combustion Including Surface Heterogeneity and Heat Generation," AIAA Journal, Vol. 4, No. 9, 1966, pp. 1629-1637. Ramohalli, K. N. R., "Steady-State Burning Propellants under Zero Cross-Flow Situation," Fundamentals SolidPropellant Combustion, edited by Kuo M. Summerfield, 90, Progress in Astronautics Aeronautics, AIAA, New York, 1984, 409-477.
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Hisao Fukunaga, Garret N. Vanderplaats, Stiffness Optimization of Orthotropic Laminated Composites Using Lamination Parameters AIAA Journal. ,vol. 29, pp. 641- 646 ,(1991) , 10.2514/3.59931
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