By Daniel P. Raymer
A superb textual content for aeronautical scholars aiming for the mainstream (ie jet-powered military/civil),industry.Not pretty much as good as Darrol Stinton's books. not anything approximately cooling liquid-cooled piston/rotary engines. The "Simplified For Hombuilders" model is sufficient for homebuilders for my part.
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Extra info for Aircraft Design: A Conceptual Approach
S^ ' 2m, V' ++ t Ru ^~ " r, n 8 and nuclei -7- ^ NR= Within the Born-Oppenheimer approximation, for which the motion of the electrons is assumed to be decoupled from the motion of the nuclei, we solve for the electronic energy as a function of nuclear position. Thus the electronic wave function is determined with the nuclear coordinates held fixed, and the only remaining two-body operator is the electronelectron repulsion term. By evaluating matrix elements of the one- and two-electron operators comprising this Hamiltonian, we obtain a two-dimensional array of one-electron integrals and a four-dimensional array of two-electron integrals, 1) di-!
The polarization CI (POL-CI) method of Hay and Dunning22-23 was designed for this purpose and has been used for a number of combustion studies involving a limited number of heavy atoms. In a POL-CI calculation, only single excitations from the reference space into the virtual space are included in the CI expansion. New CI techniques that include contributions from double excitations in an approximate way by restricting groups of configurations to appear with fixed relative importance have also been developed.
In a direct CI method, the eigenvector of the CI Hamiltonian is obtained by a scheme due to Davidson,80 where one iteratively multiplies this matrix times a trial vector. The construction and storage of the CI Hamiltonian can be avoided because only the vector resulting from the matrix multiplication is needed. 81 A CI calculation with 1 million CSF's might require an hour of CPU time on a Cray-XMP to complete. There has been a great deal of effort devoted to vectorizing these methods,82 and these schemes can be parallelized; however, there are a number of hurdles that must be overcome before very large systems can be studied.
Aircraft Design: A Conceptual Approach by Daniel P. Raymer