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Aerodynamic Control of Slender Bodies from Low to High Angles of Attack through Flow ManipulationLopera, Javier 02 July 2007 (has links)
No description available.
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Výpočet aerodynamických charakteristik nosiče pro nízkou oběžnou dráhu / Aerodynamic analysis of low orbit launcherFojtl, Michal January 2017 (has links)
Master’s thesis deals with aerodynamic heating of launch vehicle during ascent phase by using CFD simulation. Ascent trajectory and payload fairing geometry is design using data of existing small launch vehicles. Critical flight regimes are identified using 2D calculations, and in these regimes analysis is performed by axially symmetric simulations. Simulation results are compared to values obtained from theoretical and semi-empirical calculations.
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