SHOCK-BOUNDARY LAYER INTERACTION IN HYPER SONIC FLOW

Authors
GAILLARD L STORKMANN V GRONIG H
Citation
L. Gaillard et al., SHOCK-BOUNDARY LAYER INTERACTION IN HYPER SONIC FLOW, Comptes rendus de l'Academie des sciences. Serie II. Mecanique, physique, chimie, astronomie, 321(5), 1995, pp. 183-186
Citations number
4
Categorie Soggetti
Multidisciplinary Sciences
Journal title
Comptes rendus de l'Academie des sciences. Serie II. Mecanique, physique, chimie, astronomie → ACNP
ISSN journal
12518069
Volume
321
Issue
5
Year of publication
1995
Pages
183 - 186
Database
ISI
SICI code
1251-8069(1995)321:5<183:SLIIHS>2.0.ZU;2-O
Abstract
We study the hypersonic shock-flat plate boundary layer interaction. T he boundary layer separation was detected. Its length is an increasing function of the Reynolds number at the interaction point (Re-X1). Dow nstream of the interaction, crossfluctuations of hat fluxes at the wal l were observed; their amplitudes remain constant in terms of Re-X1; t heir average wavelength is invariant.