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Vink, W.J. (author), de Jonge, J.B. (author)
The present report is part of a "Manual" on aircraft loads, that is being prepared by NLR. It contains a computer program, to be used in combination with "MATLAB4 for Windows" (Student Edition) software, to study aircraft loading due to turbulence. It includes a simple aircraft response model with two rigid and three flexible symmetric degrees...
report 1997
document
Vink, W.J. (author)
In this report, a comparison is made between Doublet-Lattice and strip theory aerodynamics in symmetrical conditions of a Fokker-100-like aircraft model with rigid and flexible degrees of freedom. The generalized aerodynamic force matrices that result from the two methods show some resemblance, but this does not yield much physical insight in...
report 1996
document
de Jonge, J.B. (author), Vink, W.J. (author)
Standard methods for the calculation of Design Continuous Gust Loads cannot be applied in the case of aircraft with nonlinear response characteristics. In such cases, Design Loads can be calculated using stochastic simulation techniques. These techniques, however, require a very large computational effort. Hence, alternative methods, indicated...
report 1994