Article Comments

Contributions from readers on our articles are very welcome. This form will let us retrieve the current data in the database and allows us to consider your comments.

Effects of thermal boundary conditions on the hypersonic shock layer flow over a blunt body
Marie-Claude Druguet
International Journal of Aerodynamics (IJAD), 2012 Vol.2 No.2/3/4, pp.316 - 338
1 + 14 =

Thank you for your feedback.