J. E. Walz

发表

Structural concepts for large spacecraft

Harold G. Bush, W. L. Heard, J. E. Walz, 1980 .

Effect of orbital transfer loads on large platforms

Harold G. Bush, W. L. Heard, J. E. Walz, 1980 .

Computerized structural sizing at NASA Langley Research Center. [low mass design for aerospace vehicles]

H. G. Bush, W. J. Stroud, J. E. Walz, 1978 .

Structural sizing considerations for large space platforms

Walter L. Heard, Harold G. Bush, J. E. Walz, 1981 .

Experimental validation of optimization-based integrated controls-structures design methodology for flexible space structures

Suresh M. Joshi, Peiman G. Maghami, J. E. Walz, 1993, Proceedings of IEEE International Conference on Control and Applications.

A design technique for determining actuator gains in spacecraft vibration control

J. E. Walz, G. C. Horner, 1985 .

Deployable and erectable concepts for large spacecraft

Harold G. Bush, W. L. Heard, J. E. Walz, 1980 .

Deployable and erectable concepts for large spacecraft. [determining structural proportions of space platforms for STS delivery]

Harold G. Bush, W. L. Heard, J. E. Walz, 1980 .

Integrated design of the CSI evolutionary structure: A verification of the design methodology

Suresh M. Joshi, Peiman G. Maghami, J. E. Walz, 1993 .

Integrated controls-structures design methodology development for a class of flexible spacecraft

Suresh M. Joshi, Peiman G. Maghami, Ernest S. Armstrong, 1990 .

Structural sizing considerations for large space platforms

Walter L. Heard, Harold G. Bush, J. E. Walz, 1980 .

Stress, buckling, and vibration analysis of shells of revolution

M. S. Anderson, W. L. Heard, J. E. Walz, 1971 .

Accuracy and Convergence of Finite Element Approximations

Robert E. Fulton, J. E. Walz, R. Fulton, 1968 .