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    A finite element procedure for large deflection analysis of plates with initial deflections

    YANG, T. Y. | AIAA | 1971

    Acoustic wave amplification in solid rockets by discrete mass injection

    FLANDRO, G. A. | AIAA | 1971

    Head-end secondary flows in solid-propellant rockets due to transverse acoustic waves

    FLANDRO, G. A. | AIAA | 1971

    Particulate damping in solid propellant rockets.

    YANG, J. Y. S. | AIAA | 1972

    Buckling analysis of orthogonally stiffened waffle cylinders

    BAIG, M. I. / YANG, T. Y. | AIAA | 1974

    Flutter of Flat Finite Element Panels in a Supersonic Potential Flow

    T. Y. Yang | AIAA | 1975

    Flutter of thermally buckled finite element panels

    YANG, T. Y. / HAN, A. D. | AIAA | 1976

    Minimum weight design of an orthogonally stiffened waffle cylindrical shell with buckling constraint

    KUNOO, K. / YANG, T. Y. | AIAA | 1976

    Vibration of orthogonally stiffened waffle cylinders subjected to initial forces

    BAIG, M. I. / YANG, T. Y. | AIAA | 1976

    Reply by Author to W. P. Rodden

    T. Y. Yang | AIAA | 1977

    Finite-element panel flutter in three-dimensional supersonic unsteady potential flow

    YANG, T. Y. / SUNG, S. H. | AIAA | 1977

    Buckling of cylindrical shells with smeared-out and discrete orthogonal stiffeners

    YANG, T. Y. / KUNOO, K. | AIAA | 1977

    Minimum weight design of cylindrical shell with multiple stiffener sizes

    KUNOO, K. / YANG, T. Y. | AIAA | 1978

    Reply by Author to Rebuttal by W. P. Rodden

    T. Y. Yang | AIAA | 1979

    Flutter analysis of a NACA 64A006 airfoil in small disturbance transonic flow

    YANG, T. Y. / GURUSWAMY, P. / STRIZ, A. G. et al. | AIAA | 1980

    Minimum-mass truss structures with constraints on fundamental natural frequency

    BELLAGAMBA, L. / YANG, T. Y. | AIAA | 1981

    Boundary Condition Specification for Mobile Granular Propellant Bed Combustion Processes

    D. Y. Chen / V. Yang / K. K. Kuo | AIAA | 1981

    Flutter Analysis of MBB A-3 Supercritical Airfoil in Small Disturbance Transonic Flow

    T. Y. Yang / A. G. Striz / P. Guruswamy | AIAA | 1981

    Transonic flutter and response analyses of two 3-degree-of-freedom airfoils

    YANG, T. Y. / CHEN, C. H. | AIAA | 1982

    Application of Transonic Codes to Flutter Analysis of Conventional and Supercritical Airfoils

    T. Y. Yang / P. Guruswamy / Alfred G. Striz | AIAA | 1982

    Nonlinear panel flutter using high-order triangular finite elements

    YANG, T. Y. / HAN, A. D. | AIAA | 1983

    Buckled plate vibrations and large amplitude vibrations using high-order triangular elements

    YANG, T. Y. / HAN, A. D. | AIAA | 1983

    Transonic time-response analysis of 3-degree-of-freedom conventionaland supercritical airfoils

    YANG, T. Y. / BATINA, J. T. | AIAA | 1983

    Optimal trajectories for maximum endurance gliding in a horizontal plane

    VINH, N. X. / YANG, C.-Y. / CHERN,J.-S. | AIAA | 1984

    Application of transonic codes to aeroelastic modeling of airfoils including active controls

    BATINA, J. T. / Purdue University / West Lafayette et al. | AIAA | 1984

    A stochastic theory of fatigue crack propagation

    LIN, Y. K. / YANG, J. N. | AIAA | 1985

    Dynamics and control of lattice beams using simplified finite element models

    BERRY, D. T. / YANG, T. Y. / SKELTON, R. E. | AIAA | 1985

    Effects of viscosity and modes on transonic aerodynamic and aeroelastic characteristics of wings

    GURUSWAMY, G. P. / GOORJIAN, P. M. / MARSTILLER, J. W. et al. | AIAA | 1985

    Formulation of an imperfect quadrilateral doubly curved shell element for postbuckling analysis

    KAPANIA, R. K. / YANG, T. Y. | AIAA | 1986

    Simplified lattice beam elements for geometrically nonlinear static,dynamic, and postbuckling analysis

    BERRY, D. T. / YANG, T. Y. | AIAA | 1986

    Integrated design of space structures using lattice plate finite elements

    LAMBERSON, S. E. / YANG, T. Y. | AIAA | 1986

    Viscous effects on transonic airfoil stability and response

    BERRY, H. M. / BATINA, J. T. / YANG, T. Y. | AIAA | 1986

    Buckling, postbuckling, and nonlinear vibrations of imperfect plates

    KAPANIA, RAKESH K. / YANG, T. Y. | AIAA | 1987

    Computation of shock wave reflection by circular cylinders

    YANG, J. Y. / LIU, YEN / LOMAX, HARVARD | AIAA | 1987

    Dynamic buckling of imperfection-sensitive shell structures

    SAIGAL, SUNIL / YANG, T. Y. / KAPANIA, RAKESH K. | AIAA | 1987

    Inflation and Contact Predictions of Composite Tire Shell Carcass

    Sunil Saigal / T. Y. Yang / W. Soede | AIAA | 1987

    Numerical simulation of transient inviscid shock tube flows

    YANG, J. Y. / LOMBARD,C. K. / BERSHADER, D. | AIAA | 1987

    Elastic-plastic dynamic buckling of thin-shell finite elements with asymmetric imperfections

    YANG, T. Y. / LIAW, D. G. | AIAA | 1988

    Design of a supercritical airfoil

    ZHANG, Z. Y. / YANG, X. T. / LASCHKA, B. | AIAA | 1988

    Computational transonic flutter boundary tracking procedure

    GALLMAN, JOHN W. / YANG, T. Y. / BATINA, JOHN T. | AIAA | 1988

    Accurate rigid-body modes representation for a nonlinear curved thin-shell element

    YANG, T. Y. / KAPANIA, RAKESH K. / SAIGAL, SUNIL | AIAA | 1989

    Mach number effects on transonic aeroelastic forces and flutter characteristics

    MOHR, ROSS W. / YANG, HENRY T. Y. / BATINA, JOHN T. | AIAA | 1989

    Uniformly second-order-accurate essentially nonoscillatory schemes for the Euler equations

    YANG, J. Y. | AIAA | 1990

    A panel method for arbitrary moving boundaries problems

    YANG, J. Y. / LEE, Y. J. | AIAA | 1990

    Sequential linearization method for multilevel optimization

    VANDERPLAATS, G. N. / YANG, Y. J. / KIM, D. S. | AIAA | 1990

    Euler flutter analysis of airfoils using unstructured dynamic meshes

    RAUSCH, RUSS D. / YANG, HENRY T. Y. / BATINA, JOHN T. | AIAA | 1990

    Third-order nonoscillatory schemes for the Euler equations

    YANG, J. Y. | AIAA | 1991

    Reliability of initially compressed uncertain laminated plates in supersonic flow

    LIAW, D. G. / YANG, HENRY T. Y. | AIAA | 1991

    Reliability of uncertain laminated shells due to buckling and supersonic flutter

    LIAW, D. G. / YANG, HENRY T. Y. | AIAA | 1991

    Aeroelastic analysis of wings using the Euler equations with a deforming mesh

    ROBINSON, BRIAN A. / YANG, HENRY T. Y. / BATINA, JOHN T. | AIAA | 1991

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