Aeroelastic and Aerothermoelastic Analysis in Hypersonic Flow: Past, Present, and Future

By Jack J. McNamara, Peretz P. Friedmann. 2011

293 citations recorded by the source corpus.

Subfields: Applied Mathematics, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/1e32ceac9acb85f26e30ea8d28553830b5ef5aee

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Applied Mathematics

1. Adam J. Culler
2. Jack J. McNamara

In Computational Mechanics

1. Jack J. McNamara
2. Adam J. Culler
3. Peretz P. Friedmann

Citations in the corpus

• Impact of Fluid-Thermal-Structural Coupling on Response Prediction of Hypersonic Skin Panels (2011, methodology): “While piston theory represents a simplistic model for the inviscid aerodynamics, it has been observed in several studies [13] to provide reasonably accurate pressure predictions so long as the product of Mach number and surface inclination remains below unity.”