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Dive into the research topics where Bruno Le Naour is active.

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Featured researches published by Bruno Le Naour.


16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference | 2009

R&T Effort on Pulsed and Continuous Detonation Wave Engines

Francois Falempin; Bruno Le Naour

Due to its thermodynamic cycle, the pulsed detonation engine (PDE) has theoretically a higher performance than classical iso-pressure combustion propulsion concepts. Nevertheless, PDE design must avoid this advantage being not fully compensated by the difficulties encountered for practical use of the PDE concept or by the complex technology, which could be needed to implement it in an operational flying system, particularly due to severe generated vibration environment. The Continuous Detonation Wave Engine (CDWE) can also be considered to reduce the environmental conditions generated by PDE while reducing the importance of initiation issue and simplifying some integration aspects. Specific experimental program has been performed by MBDA and Lavrentiev Institute to understand unsteady, three dimensional flow behind the detonation wave and to address some key points for the feasibility of an operational rotating wave engine for space launcher. On the basis of these results, a preliminary design of an operational engine has been performed by taking into account all engine/airframe integration issues in order to optimize the ben efit of detonation wave engine. Beyond these first steps, MBDA designed a large scale ground demonstrator allowing to address all issues for a continuous detonation rocket engine using LH2/LOx mixture. As a first step toward the development of this large scale engine, a small scale demo is to be tested in Fall 2009.


17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference | 2011

Recent experimental results obtained on Continuous Detonation Wave Engine

Bruno Le Naour; Francois Falempin; Flore Miquel

Due to its thermodynamic cycle, the Continuous Detonation Wave Engine has theoretically a higher performance than classical iso-pressure combustion propulsion concepts. CDWE can also be considered to reduce the environmental conditions generated by other detonation engines such as PDE while reducing the importance of initiation issue and simplifying some integration aspects. After performing some specific experimental and numerical programs at LIH, MBDA designed a preliminary demonstrator of CDWE with the support of the EADS Nursery. A first assessment of the tests in progress is presented in the following article.


21st AIAA International Space Planes and Hypersonics Technologies Conference | 2017

MBDA R&T Effort Regarding Continuous Detonation Wave Engine for Propulsion - Status in 2016

Bruno Le Naour; Francois Falempin; Kevin Coulon


Archive | 2012

TURBINE ENGINE INCLUDING A DETONATION CHAMBER AND AIRCRAFT PROVIDED WITH SUCH A TURBINE ENGINE

Francois Falempin; Bruno Le Naour


Archive | 2012

Ramjet including a detonation chamber and aircraft comprising such a ramjet

Francois Falempin; Bruno Le Naour


21st AIAA International Space Planes and Hypersonics Technologies Conference | 2017

Bladeless turbines for unsteady high speed flows

Francois Falempin; Guillermo Paniagua Perez; James Braun; Bruno Le Naour


Archive | 2012

Turbine engine including a continuous wave detonation chamber and cooling bypass flow and aircraft provided with such a turbine engine

Francois Falempin; Bruno Le Naour


Archive | 2012

Ramjet engine with detonation chamber and aircraft comprising such a ramjet engine

Francois Falempin; Bruno Le Naour


Archive | 2011

Application of Continuous Detonation Wave Concept to Turbojet Engine

Francois Falempin; Bruno Le Naour


Archive | 2009

A Contribution to the Development of Actual Pulsed and Continuous Detonation Wave Engines

Francois Falempin; Bruno Le Naour

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