Results 241 to 250 of about 19,118 (298)
Some of the next articles are maybe not open access.

Greenization Factor of a Turbojet Engine

2017
[No abstract available]
Şöhret, Yasin, Karakoç, Tahir Hikmet
openaire   +2 more sources

Effects of isentropic efficiency of turbomachinery components on entropy production for small turbojet engine

, 2021
Purpose Usage of gas turbine engines has increased by day due to rising demand for military and civil applications. This case results in investigating diverse topics related to energy efficiency and irreversibility of these systems.
Hakan Aygün
semanticscholar   +1 more source

Investigation of Novel Thrust Parameters to Variable Geometry Turbojet Engines

International Symposium on Applied Machine Intelligence and Informatics, 2021
Although propulsion systems in commercial aviation rely on high bypass ratio turbofan engines, there is still a niche in which turbojet engines can be utilized.
K. Beneda
semanticscholar   +1 more source

Afterburners for Turbojet Engines

Journal of the Aeronautical Sciences, 1948
The general problem of pure jet aircraft take-off distance is indicated, and the basic reasons for the excess-thrust deficiency as compared to propeller aircraft are shown. The inherent advantages and disadvantages of several methods of short-duration thrust augmentation, such as fluid injection or rocket boosters, to alleviate the difficulties are ...
openaire   +2 more sources

Biofueled Miniature Turbojet Engine (BIOMITE) [PDF]

open access: possible50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2012
The Busemann Advanced Concepts Lab at the University of Colorado Boulder has been researching improvements to small turbojet engines designed for unmanned aerial vehicles for the past three years. The BIOMITE senior design team has continued this tradition by designing adaptations for a commercial-off-the-shelf US Microjet AT-450 turbojet engine to run
Donald S. Gipe   +2 more
openaire   +1 more source

Turbojet Engine Simulation Using Dymola [PDF]

open access: possible42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2006
This work describes the development of a global model of a modified turbojet engine for dynamic behavior simulation. The Modelica language is used for the simulation of this model. A Modelica package was created for the basic components suitable for such models. The model is based on a general turbojet engine and a turbofan engine. The engine component
Abdollah A. Afjeh   +2 more
openaire   +1 more source

Turbojet engine innovation and TRIZ

Proceedings of the 16th International Conference on Mechatronics - Mechatronika 2014, 2014
Comparing to concurrent small turbojet engines this Czech design has several important parametrical advantages: weight, power, reliability, cost, etc. Innovations were obtained by creative/inventive solutions in which several instruments TRIZ were used objectively.
Zdenek Katolicky   +2 more
openaire   +2 more sources

Exergetic, Exergoeconomic, Sustainability and Environmental Damage Cost Analyses of J85 Turbojet Engine with Afterburner

, 2020
This paper deals with the performance analyses of exergetic, exergoeconomic, sustainability and environmental damage cost for J85 turbojet engine at Idle (ID), Intermediate (INT), Military (MIL) and Afterburner (AB) operation modes.
Ozgur Balli
semanticscholar   +1 more source

Noise From Turbojet Compressors

The Journal of the Royal Aeronautical Society, 1964
SummaryThe noise radiated from the intakes of turbojet engines during landing is already causing a serious nuisance. This paper, which is largely based on the deliberations of an ad hoc working panel of academic experts formed by Rolls-Royce in 1961, describes the characteristics of the noise and discusses possible mechanisms of generation.
R. Bridge, S. L. Bragg
openaire   +2 more sources

Characterization of the Wear in the Turbojet Fins

Key Engineering Materials, 2015
The wear is very difficult to characterize because of its complexity and its measurement phenomenon. Our work is to prepare samples Fan blades, worn, to determine the nature of the wear and damage them. For these reasons, the characterization of these samples was conducted in different microscopic and macroscopic scales.
Djamel Guechi, Necib Brahim, Zohra Labed
openaire   +2 more sources

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