HYBRID METHOD FOR RAPID PROTOTYPING OF CORE MODELS OF AIRCRAFT ENGINE BLADES - Europub

Search

Apply

HYBRID METHOD FOR RAPID PROTOTYPING OF CORE MODELS OF AIRCRAFT ENGINE BLADES

Journal Title: Journal of KONES - Year 2012, Vol 19, Issue 2

Abstract

Authors and Affiliations

Grzegorz Budzik, Krzysztof Kubiak, Jacek Bernaczek, Marek Magniszewski, Hubert Matysiak, Rafał Cygan, Marcin Tutak

Keywords

engine blades precise casting rapid prototyping directional crystallization

Related Articles

PROBLEMS OF COOPERATIVE INTELLIGENT TRANSPORT SYSTEMS (ITS) IMPLEMENTATION IN EUROPEAN UNION

ATTEMPT OF INJECTORS FAILURE DETECTION BASED ON MEASUREMENT OF THE ANGULAR SPEED DISCRETE VALUE

THE POSSIBILITIES OF EARLY FAULT DETECTION OF ENGINES

CHOSEN ASPECTS OF SIMULATION MODEL TO DESIGNING PRO-ECOLOGICAL TRANSPORT SYSTEM

A COMPARISON OF BURNING CHARACTERISTICS OF ISO-OCTANE AND ETHANOL FUELS IN AN OPTICAL SI ENGINE

Download PDF file

EP ID EP71134
DOI 10.5604/12314005.1137895
Views 99
Downloads 0

How To Cite

Grzegorz Budzik, Krzysztof Kubiak, Jacek Bernaczek, Marek Magniszewski, Hubert Matysiak, Rafał Cygan, Marcin Tutak (2012). HYBRID METHOD FOR RAPID PROTOTYPING OF CORE MODELS OF AIRCRAFT ENGINE BLADES. Journal of KONES, 19(2), 77-82. https://europub.co.uk./articles/-A-71134