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Letter 5090
Material Properties of
NarLoy-Z
.
We analyze rocket combustion chambers (such as the Vulcain-Engine
of the Ariane Rocket) numerically with a Finite Element Program.
For this purpose, we need to know e.g. a few material properties
of NarLoy-Z (such as modulus of elasticity, yield stress, hardening
module) in dependence on the temperature. Do you know anyone (or a
publication) where we could get this information from? In order to
validate our calculation methods, we are going to build a model
combustion chamber, possibly from Narloy-Z.
How much is this Material (per kg) and where may we get it from?
J–rg Richard Riccius
German Aerospace Research Center
DLR - Lampoldshausen, Ba-Wue, Germany
+
I have exactly the same problem that you and I have found out the
reference of a publication.
I am trying to get it, so I don't realy know if it is what you are
looking for.
I hope it will be useful:
- "Journal of Material Science"
- Subject: Chemical Sciences
- ISSN:022-2461
- Volume 32 Issue 14 (1997) pp 3891-3903
- Publication Date 01/01/1997 (printed version)
- Title: "Mechanical properties and microstructural stability of
wrought, laser, and electron beam glazed NARloy-Z alloy at
elevated temperatures"
If could foud yet these data by another way, could you please let
me know.
Paloma de la PeÒa
GarcÌa
- Madrid,Spain
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