Experimental study on the PRE-X vehicle focusing on the transitional shock-wave/boundary-layer interactions

Author:

Bur R.,Chanetz B.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference13 articles.

1. Shock-wave transitional boundary-layer interactions in hypersonic flow;Benay;AIAA Journal,2006

2. R. Bur, Y. Le Sant, B. Chanetz, Experimental study of the PRE-X re-entry vehicle in R2Ch wind tunnel, in: 1st International Symposium on ARA Days — Atmospheric Re-entry Systems, Missions and Vehicles, Arcachon, France, July 3–5, 2006

3. R. Bur, Y. Le Sant, L. Morzenski, AVP-RE-2310000-01-ONER-01: PRE-X — Phase A2 — R2Ch wind tunnel tests campaign: Tests Report, ONERA Report RT 1/10231 DAFE, September 2005

4. Experimental and numerical study of the laminar separation in hypersonic flow;Chanetz;Aerospace Science and Technology,1998

5. Etude expérimentale de l'interaction onde de choc/couche limite en écoulement hypersonique;Coët;La Recherche Aérospatiale,1993

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