Showing papers by "Robert M. Bennett published in 1998"
15 Jun 1998
TL;DR: The motivation for CA and the elements of one type of the analysis or simulation process are briefly reviewed in this article, and the need for streamlining and improving the overall process to reduce elapsed time and improve overall accuracy is discussed.
Abstract: The motivation for Computational Aeroelasticity (CA) and the elements of one type of the analysis or simulation process are briefly reviewed The need for streamlining and improving the overall process to reduce elapsed time and improve overall accuracy is discussed Further effort is needed to establish the credibility of the methodology, obtain experience, and to incorporate the experience base to simplify the method for future use Experience with the application of a variety of Computational Aeroelasticity programs is summarized for the transonic flutter of two wings, the AGARD 4456 wing and a typical business jet wing There is a compelling need for a broad range of additional flutter test cases for further comparisons Some existing data sets that may offer CA challenges are presented
93 citations