High Frequency Combustion Instabilities in the DVRC Rocket Combustor : Experimental Study of Combustion Instabilities in a Liquid Rocket Engine

Language: English

Published by LAP LAMBERT Academic Publishing, 2014

3659639168 / 9783659639166

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Seller: AHA-BUCH GmbH, Einbeck, GermanyAHA-BUCH GmbH

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nach der Bestellung gedruckt Neuware - Printed after ordering - This experimental work regards the studies of the high frequency combustion instabilities inside the DVRC (Discretely Variable Resonance Combustor), a liquid rocket engine, developed by the Purdue University at M. J. Zucrow Laboratories, on behalf of Nasa Marshall Space Flight Center. The research revealed that, given these specific flow conditions, combustion instability occurs inside the system during hot fire tests. The most important experimental result of the study showed the oxidizer manifold acting as a damper of the pressure oscillations coming from the combustion chamber and how this can represent an advantage in terms of reduced mechanical loads at the interface with the rest of the feed system. The LEE code based on the linearized Euler equations detected both the combustion instability inside the DVRC and confirmed the positive role of the oxidizer manifold. The best agreement with the experimental results has been observed considering heat addition at the plane of propellants injection into the combustion chamber, showing it is reasonable to assume combustion occurs mainly in proximity of that plane, as the previous works about CVRC and CFD results had already shown.…

Seller Inventory # 9783659639166

Title
High Frequency Combustion Instabilities in the DVRC Rocket Combustor : Experimental Study of Combustion Instabilities in a Liquid Rocket Engine
Author
Andrea Terracciano
Publisher
LAP LAMBERT Academic Publishing
Publication year
2014
Condition
Neu
Binding
Taschenbuch
Language
English
ISBN 10
3659639168
ISBN 13
9783659639166
Item weight
322 grams
Dimensions
220x150x13 mm

AHA-BUCH GmbH

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