Skip to main content
Book Chapter

Aerodynamic Ground Effect for Transonic Projectiles

  • Kleine H
  • Young J
  • Oakes B
  • et al.
Springer Berlin Heidelberg, (2012), 519-524
DOI: 10.1007/978-3-642-25685-1_78
N/ACitations
Citations of this article
7Readers
Mendeley users who have this article in their library.
Get full text

Abstract

The aerodynamic characteristics of an object flying in close proximity to a solid surface are altered by the presence of this boundary. This phenomenon, known as aerodynamic ground effect, has been thoroughly investigated in the subsonic flow regime [1], but to the...

Cite

CITATION STYLE

APA

Kleine, H., Young, J., Oakes, B., Hiraki, K., Kusano, H., & Inatani, Y. (2012). Aerodynamic Ground Effect for Transonic Projectiles. In 28th International Symposium on Shock Waves (pp. 519–524). Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-25685-1_78

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Save time finding and organizing research with Mendeley

Sign up for free