I. Lottati

发表

Application of the aerodynamic energy concept to flutter suppression and gust alleviation by use of active controls

E. Nissim, A. Caspi, I. Lottati, 1976 .

Active Controls for Flutter Suppression and Gust Alleviation in Supersonic Aircraft

E. Nissim, I. Lottati, I. Lottati, 1980 .

An Optimization Method for the Determination of the Important Flutter Modes

E. Nissim, I. Lottati, 1981 .

Aeroelastic stability characteristics of a composite swept wing withtip weights for an unrestrained vehicle

I. Lottati, I. Lottati, 1987 .

Aeroelastic tailoring of a composite wing with a decoupler pylon as a wing/store flutter suppressor

I. Lottati, 1988 .

The Role of Structural and Aerodynamic Damping on the Aeroelastic Behavior of Wings

I. Lottati, 1986 .

Induced drag and lift of wing by the piecewise continuous kernel function method

I. Lottati, I. Lottati, 1984 .

A Finite-Volume Algorithm for Three-Dimensional Magnetohydrodynamics on an Unstructured, Adaptive Grid in Axially Symmetric Geometry

I. Lottati, Dalton D. Schnack, P. Satyanarayana, 1998 .

Active External Store Flutter Suppression in the YF-17 Flutter Model

E. Nissim, I. Lottati, I. Lottati, 1979 .

Three-Dimensional Oscillatory Piecewise Continuous-Kernel Function Method—Part I: Basic Problems

E. Nissim, I. Lottati, I. Lottati, 1981 .

The role of damping on supersonic panel flutter

I. Lottati, 1985 .

Three-dimensional oscillatory piecewise continuous-kernel function method. I - Basic problems. II - Geometrically continuous wings. III - Wings with geometrical discontinuities

E. Nissim, I. Lottati, I. Lottati, 1981 .

Flutter and divergence aeroelastic characteristics for composite forward swept cantilevered wing

I. Lottati, I. Lottati, 1985 .

Three-Dimensional Oscillatory Piecewise Continuous-Kernel Function Method-Part II: Geometrically Continuous Wings

E. Nissim, I. Lottati, I. Lottati, 1981 .

Supersonic three-dimensional oscillatory piecewise continuous kernelfunction method

E. Nissim, I. Lottati, I. Lottati, 1983 .