REFINED HIGHER ORDER FINITE ELEMENT MODELS FOR THERMAL BUCKLING OF LAMINATED COMPOSITE AND SANDWICH PLATESC. Sarath Babu, T. Kant, · Journal of Thermal Stresses · 2000

A higher order finite element theory for buckling and vibration analysis of initially stressed composite sandwich platesA.K. Nayak; S.S.J. Moy; R.A. Shenoi · 2005

[American Institute of Aeronautics and Astronautics 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit - Long Beach,CA,U.S.A. (20 April 1998 - 23 April 1998)] 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit - A higher order finite element for sandwich platesOskooei, S.; Hansen, J. · 1998

Tensile failure of fibrous compositesROSEN, B. W. · AIAA Journal · 1964

Vibrational nonequilibrium effects on diatomic dissociation ratesAIAA Journal · 1993

Transonic Helicopter NoiseMorgans, Aimee S.; Karabasov, Sergey A.; Dowling, Ann P.; Hynes, Tom P. · AIAA Journal · 2005

Versatile Kirchhoff Code for Aeroacoustic PredictionsLyrintzis, A.; Xue, Y. · AIAA Journal · 1997

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Review of "Vibration of Mechanical Systems"Marie, Hazel · AIAA Journal · 2011

Optical Measurements of Muzzle BlastSchmidt, E. M.; Shear, D. · AIAA Journal · 1975

Noise of Swirling Exhaust JetsLu, H.Y.; Ramsay, J.W.; Miller, D.L. · AIAA Journal · 1977