Viscous shock layer around slender bodies with nonequilibrium air chemistry
A method has been developed which can reliably compute nonequilibrium viscous shock
layer over blunt-nosed bodies. This method considerably improves computational efficiency …
layer over blunt-nosed bodies. This method considerably improves computational efficiency …
[PDF][PDF] Approximate Viscous Shock-Layer Analysis of Axisymmetric Bodies in Perfect Gas Hypersonic Flow
S Ghasemloo, S Noori - Journal of Space Science and Technology, 2014 - jsstpub.com
In this paper, an approximate axisymmetric method is developed which can reliably
calculate fully viscous hypersonic flow over blunt-nosed bodies. In this method, a Maslen's …
calculate fully viscous hypersonic flow over blunt-nosed bodies. In this method, a Maslen's …
[PDF][PDF] Fuzzy Sliding Mode for Spacecraft Formation Control in Eccentric Orbits
J perturbation and atmospheric drag are considered as external disturbances. Using the
Lyapunov second method, the stability of the closed-loop system is guaranteed. The …
Lyapunov second method, the stability of the closed-loop system is guaranteed. The …
[PDF][PDF] Laminar and Turbulent Aero Heating Predictions over Blunt Body in Hypersonic Flow
SA Hosseini, S Noori - علوم و فناوری فضایی, 2014 - jsstpub.com
In the present work, an engineering method is developed to predict laminar and turbulent
heating-rate solutions for blunt reentry spacecraft at hypersonic conditions. The calculation …
heating-rate solutions for blunt reentry spacecraft at hypersonic conditions. The calculation …