J. Archambaud

发表

Natural Transition in Supersonic Flows: Flat Plate, Swept Cylinder, Swept Wing

Daniel Arnal, Gerald Carrier, Jean-Pierre Archambaud, 2004 .

Influence of Surface Roughness and of Suction on the Receptivity of a Swept Wing Boundary Layer

D. Arnal, A. Séraudie, J. Archambaud, 2000 .

Transition Control Testing in the Supersonic S2MA Wind Tunnel (SUPERTRAC project)

J. Godard, R. Donelli, A. Hanifi, 2010 .

Automatic Transition Predictions Using Simplified Methods

Raffaele Donelli, Daniel Arnal, Jean Perraud, 2009 .

Active Control Technology for Enhanced Performance Operational Capabilities of Military Aircraft, Land Vehicles and Sea Vehicles

Anuradha M. Annaswamy, G. S. Samuelsen, M. F. Golnaraghi, 2001 .

Automatic Transition Predictions Using Simplified Methods

Raffaele Donelli, Daniel Arnal, Jean Perraud, 2009 .

Boundary layer transition analysis on NEXST-1 airplane: NAL-ONERA cooperative research project

D. Arnal, A. Séraudie, N. Tokugawa, 2007 .

USE OF ADAPTIVE WALLS IN 2D TESTS

J. P. Archambaud, J. P. Chevallier, J. Archambaud, 1984 .