These proceedings collect the 37 theses presented at the 6th NAL Symposium on Aircraft Computational Aerodynamics held by National Aerospace Laboratory in June, 1988. The main theses, among others, comprise 9 theses of simulation of supersonic turbulent flow action about winged body, 7 theses of numerical analysis to obtain more accurate solution of Navier-Stokes equation, 4 theses of study of combustion in gas turbine and jet engine, 4 theses of numerical analysis of flow around transonic aircraft, 4 theses of study of hypersonic viscous flow around space plane and 4 theses of aerodynamical calculation of space plane, which are result reports of use of TV, TVD and ATVD2 schemes as calculation methods for the transition from the transonic zone to the supersonic zone. Apart from those theses, the visualization of computed unsteady flow in three dimensions and prototypical production to develop a new supercomputer utilizing the parallel computer, among others, were reported. 261 refs., 295 figs., 7 tabs.
Dai 6 kai kokuki keisan kuki rikigaku symposium ronbunshu. (Special publication of National Aerospace Laboratory. Proceedings at the 6th NAL symposium on aircraft computational aerodynamics)
1988
252 pages
Report
Keine Angabe
Englisch