| Nota(s) | Request for Nomination of articles for the Special 100th Anniversary of Flight Issue, p.1; Announcements and Acknowledgments, p.2; Editorial Policy Statement on Numerical Accuracy and Experimental Uncertainty, p.10; Reviewers for 1 October 1998-30 September 1999, p.11; Staggered-Mesh computation for aerodynamic Sound, p.16; Numerical Solution of Acoustic Propagation Problems Using Linearized Euler Equations, p.22; Impedance and Its Time-Domain Extensions, p.30; Four-Channel Suction Distribution Optimization Experiments for Laminar flow control, p.39; Inverse solution Uniqueness and Domain of Existence for Space-Marching Applications, p.44; Finite element Adaptive multigrid Euler Solver for Rotary Wing Aerodynamics, p.50; Rotor Wake Modeling for Flight Dynamic Simulation of Helicopters, p.57; Effects of Injection Angle on Atomization of Liquid Jets in Transverse Airflow, p.64; Direct Numerical Simulation and Modeling of a Nonequilibrium turbulent Plasma, p.73; Two Interacting Vortex Ring Pairs and Their Sound Generation, p.79; Turbulence Effect on Frequency Characteristics of Unsteady motions in wake of Wing, p.87; Measurement of Transient Temperature field Within a Falling Droplet, p.95; Investigation of Equivalent System Modeling and Dynamic Characteristics Using Reduced models, p. 102; Strength Prediction of Fiber Reinforced Plastics with a Hole Under Compression-Tension, p.110; Sensitivity Derivatives of Eigendata of One-Dimensional Structural System, p.115; Combined finite element Analysis and Statistical energy Analysis in Mechanical Intensity Calculations, p.123; Multibody implementation of finite Volume C beams, p.131; Structural Modeling of Parachute dynamics, p.139; Redesigning the Dynamics of Structural systems, p. 147; From Dubious Construction of Objective Functions to the Application of Physical Programming, p.155; Bilevel Integrated System Synthesis, p. 164; Aerodynamic Design Using Neural Networks, p.173
Request for Nomination of Articles for the Special 100th Anniversary of Flight Issue, p. 1; Announcements and Acknowledgments, p.2; Reviewers for 1 October 1998-30 September 1999, p.11: Staggered-Mesh Computation for Aerodynamic Sound, p.16; Numerical Solution of Acoustic Propagation Problems Using Linearized Equations, p.22;Impredance and its time-Domain Extensions, p.30; Four- Channel Suction Distribution Optimization Experiments for Laminar flow Control, p.39; Inverse Solution Uniqueness and Domain of Existence for Space-Marching Applications, p.44; Finite Element Adaptive Multigrid Euler Solver for Rotary Wing Aerodynamics, p.50; Rotor Wake Modeling for flight Dynamic Simulation of Helicopters, p.57; Effects of Injection Angle on Atomization of Liquid Jets in Transverse Airflow, p.64; Direct Numerical Simulation and Modeling of a Nonequilibrium Turbulent Plasma, p.73; Two Interacting Vortex Ring Pairs and Their Sound Generation, p.79; Turbulence Effect on Frequency Characteristics of Unsteady Motions in Wake of Wing, p.87; Measurement of Transient Temperature Field Within a Falling Droplet, p.95; Investigation of Equivalent System Modeling and Dynamic Characteristics Using Reduced Models, p.102; Strength Prediction of Fiber Reinforced Plastics with a hole Under Compression-Tension, p.110; Sensitivity of Eigendata of One-Dimensional Structural Systems, p.115; Combined Finite element Analysis and Statistical energy Analysis in Mechanical Intensity Calculations, p.123; Multibody Implementation of Finite volume C° Beams, p.131; Structural Modeling of Parachute Dynamics, p.139; Redesigning the Dynamics of Structural Systems, p.147; From Dubious Construction of Physical Programming, p.155; bilevel Integrated System Synthesis, 164; Aerodynamic Design Using Neural Networks, p.173; Shaping of Delta-Wing Planform to Suppress Vortex Breakdown, p.183; Surface Shaping to Suppress Vortex Breakdown on Delta Wings, p.186.
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