Assessing Hypersonic Boundary-Layer Stability in the Presence of Structural Deformation

This work investigates the effect of two-dimensional surface deformations on hypersonic boundary-layer stability. The deformations are obtained from previous research and represent the characteristic response of integrated thermal protection system panels due to combined aerodynamic and thermal load...

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Veröffentlicht in:	AIAA journal 2014-11, Vol.52 (11), p.2547-2558
Hauptverfasser:	Riley, Zachary B, McNamara, Jack J, Johnson, Heath B
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamic stability Aerodynamics Aerospace engineering Boundaries Boundary conditions Boundary layer Boundary layer transition Deformation Deformation effects Dimensional stability Dynamical systems Dynamics Hypersonic flow Mach number Panels Parabolized stability equations Stability Stability analysis Surface stability Thermal protection
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