Skip to main content
Book Chapter

Wave drag reduction by means of aerospikes on transonic wings

  • Rein M
  • Rosemann H
  • Schülein E
Springer Berlin Heidelberg, (2009), 1309-1313
DOI: 10.1007/978-3-540-85181-3_83
N/ACitations
Citations of this article
9Readers
Mendeley users who have this article in their library.
Get full text

Abstract

Wave drag and shock induced boundary layer separation are important issues of flows around transonic wings. At transonic speeds the supersonic flow regime that is formed locally above wings, is terminated by a shock wave. This happens especially under off-design...

Cite

CITATION STYLE

APA

Rein, M., Rosemann, H., & Schülein, E. (2009). Wave drag reduction by means of aerospikes on transonic wings. In Shock Waves (pp. 1309–1313). Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-85181-3_83

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