Aeromechanics and Vehicle Configuration Demonstrations. Volume 2: Understanding Vehicle Sizing, Aeromechanics and Configuration Trades, Risks, and Issues for Next-Generations Access to Space Vehicles
Aeromechanics and Vehicle Configuration Demonstrations. Volume 2: Understanding Vehicle Sizing, Aeromechanics and Configuration Trades, Risks, and Issues for Next-Generations Access to Space Vehicles
- Neue Suche nach: D. Crowley
- Neue Suche nach: S. Edwards
- Neue Suche nach: D. Mavris
- Neue Suche nach: D. Crowley
- Neue Suche nach: S. Edwards
- Neue Suche nach: D. Mavris
This volume describes the work performed for Task C - Creation of Multi-fidelity Aerodynamic Analysis Tool. This task focuses on the development of a methodology employing contour-based sampling and multi-fidelity modeling in the creation of aerodynamic surrogate models. The methodology is successfully demonstrated for a parametric reusable booster vehicle.
Dokumentinformationen
Aeromechanics and Vehicle Configuration Demonstrations. Volume 2: Understanding Vehicle Sizing, Aeromechanics and Configuration Trades, Risks, and Issues for Next-Generations Access to Space Vehicles
2014
259 pages
Report
Keine Angabe
Englisch
Operations Research , Rocket Engines & Motors , Spacecraft Trajectories & Flight Mechanics , Aerodynamics , Boost glide vehicles , Computation science , Computerized simulation , Flight simulation , Recoverable booster engines , Reusable equipment , Sampling , Uncertainty , Adaptive sampling , Rbs(Reusable booster system) , Surrogate modeling , Hlv(Hybrid launch vehicle) , Conceptual level return trajectories , Glide back trajectories , Early phase systems engineering , Design studies , Contour based sampling , Aeromechanics , Vehicle configuration tradespace
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