Transition measurement and analysis on a swept wing in high lift configuration-Reference-Cited by-同舟云学术

Transition measurement and analysis on a swept wing in high lift configuration

Published:2003-12 Issue:8 Volume:7 Page:569-576
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Séraudie A.,Perraud J.,Moens F.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference11 articles.

1. Leading edge contamination and relaminarisation on a swept wing at incidence;Arnal,1989

2. Transition prediction in transonic flows;Arnal,1988

3. J.A. Beasley, Calculation of the laminar boundary layer and prediction of transition on a sheared wing, RAE Farnborough, Report No 3787, 1976

4. Assessment of elsA software through civil transport aircraft configurations;Ben Kheli,2002

5. G. Casalis, D. Arnal, Database method – Development and validation of the simplified method for pure crossflow instability at low speed, ELFIN II Subtask 2.3, ELFIN II Tech. Rep. No 145, 1996

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