The objective of this thesis is to design and assemble a test rig able of both the assessment of on-ground performances and the analysis of the thermodynamic cycle of any given micro-turbojet engine. The latter requires the rig to be capable of measuring a set of physical quantities across the whole range of working conditions in order to asses component performances and efficiencies. Furthermore, this thesis will provide new equipment to the university and enable future works as it will be possible to perform studies with these type of engines or measure and quantify any modifications and improvements implemented in future theses. The present design, commission and assembly builds upon prior preliminary work on the expected thermodynamic c...
A test stand was developed to evaluate an 11.5 cc, two-stroke, internal combustion engine in anticip...
Copyright © 2013 Alfonso Calabria et al. This is an open access article distributed under the Creati...
This article describes the multi-level approach to developing the virtual testing rig of gas turbine...
Thesis (M.Ing. (Computer and Electronical Engineering))--North-West University, Potchefstroom Campus...
In this project, a general-purpose ground level jet engine test cell was designed and developed. The...
This paper describes the development of experimental testing system and performance measurement of s...
Abstract — The reason behind doing this work was to prepare an experimental procedure of a micro tur...
During the forthcoming years many new aircrafts such as A350 and B787 are being designed and continu...
Good estimation of aerodynamic coefficients is of fundamental importance in the design and developme...
This work will be focused on issue of a jet engine. The thesis will be divided into search retrieval...
Nanyang Technological University (NTU) has grown her interest in developing, designing and manufactu...
In 1997 the Turbomachinery Group of the University of Liege decided to acquire a small jet engine to...
[[abstract]]A miniature turbojet engine was developed for the Unmanned Aerial Vehicle (UAV) applicat...
The ever increasing development of portable electronics has led to a higher demand for compact and r...
Microjet engines have gone from being developed in private workshops meant for the RC model aircraft...
A test stand was developed to evaluate an 11.5 cc, two-stroke, internal combustion engine in anticip...
Copyright © 2013 Alfonso Calabria et al. This is an open access article distributed under the Creati...
This article describes the multi-level approach to developing the virtual testing rig of gas turbine...
Thesis (M.Ing. (Computer and Electronical Engineering))--North-West University, Potchefstroom Campus...
In this project, a general-purpose ground level jet engine test cell was designed and developed. The...
This paper describes the development of experimental testing system and performance measurement of s...
Abstract — The reason behind doing this work was to prepare an experimental procedure of a micro tur...
During the forthcoming years many new aircrafts such as A350 and B787 are being designed and continu...
Good estimation of aerodynamic coefficients is of fundamental importance in the design and developme...
This work will be focused on issue of a jet engine. The thesis will be divided into search retrieval...
Nanyang Technological University (NTU) has grown her interest in developing, designing and manufactu...
In 1997 the Turbomachinery Group of the University of Liege decided to acquire a small jet engine to...
[[abstract]]A miniature turbojet engine was developed for the Unmanned Aerial Vehicle (UAV) applicat...
The ever increasing development of portable electronics has led to a higher demand for compact and r...
Microjet engines have gone from being developed in private workshops meant for the RC model aircraft...
A test stand was developed to evaluate an 11.5 cc, two-stroke, internal combustion engine in anticip...
Copyright © 2013 Alfonso Calabria et al. This is an open access article distributed under the Creati...
This article describes the multi-level approach to developing the virtual testing rig of gas turbine...