The "Supersonic Aerodynamics" Project at ONERA

Topics:
Aerospace and Defense
Tags:
Construction,
ONERA
Source:
ONERA

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Overview: The paper provides an overview of the current work performed in the framework of this project. Five problems are investigated: - Laminar-turbulent transition and laminar flow control: an experimental database for 3D transition has been obtained; in parallel, the prediction codes developed for low speed flows are extended to supersonic configurations. - Development of a "quiet" supersonic wind tunnel: the suction device in the R1Ch wind tunnel has been improved, so that laminar flow was observed on the nozzle wall downstream of the throat. - Compressible turbulent flows at high.

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Format: PDF | Size: 3,625KB | Date: Oct 2002 | Pages: 14

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