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- W2313804950 abstract "The unsteady flowfield of a realistic two-stage hypersonic vehicle during the separation process is investigated. In particular, the aerodynamic characteristics of the orbital stage in the first phase of the separation are addressed. The numerical simulations of these first investigations are based on a finitevolume method solving the three-dimensional unsteady Euler equations. The results focus on the flow fields and the pressure distributions as well as on the aerodynamic coefficients. The latter provides an essential mean for the stability and control evaluations. The analysis shows that unsteadiness cannot be neglected. List of Symbols c e Q F,G,H u,v,w" @default.
- W2313804950 created "2016-06-24" @default.
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- W2313804950 date "2001-04-24" @default.
- W2313804950 modified "2023-09-26" @default.
- W2313804950 title "Unsteady aerodynamics of a hypersonic vehicle during a separation phase" @default.
- W2313804950 cites W2064370164 @default.
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- W2313804950 doi "https://doi.org/10.2514/6.2001-1852" @default.
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